{"id":18,"date":"2023-03-22T18:42:13","date_gmt":"2023-03-23T01:42:13","guid":{"rendered":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/?page_id=18"},"modified":"2026-04-22T05:47:43","modified_gmt":"2026-04-22T12:47:43","slug":"publications","status":"publish","type":"page","link":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/publications\/","title":{"rendered":"Publications"},"content":{"rendered":"<p><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-60\" src=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-375x500.jpg\" alt=\"\" width=\"375\" height=\"500\" srcset=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-375x500.jpg 375w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-1125x1500.jpg 1125w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-750x1000.jpg 750w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-1152x1536.jpg 1152w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-1536x2048.jpg 1536w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-26-23.26.52-scaled.jpg 1920w\" sizes=\"auto, (max-width: 375px) 100vw, 375px\" \/><\/p>\n<p><strong>Textbooks<\/strong><\/p>\n<p>1.\u00a0\u00a0\u00a0\u00a0\u00a0<strong>Takahashi, T.T.<\/strong>, Aircraft Performance &amp; Sizing, Vol. I: Fundamentals of Aircraft Performance, Momentum Press, New York, NY, 2016. 200 pages.\u00a0<strong>ISBN-13:<\/strong>\u00a0978-1606506837<\/p>\n<p>2.\u00a0\u00a0\u00a0\u00a0\u00a0<strong>Takahashi, T.T.<\/strong>, Aircraft Performance &amp; Sizing, Vol. II: Applied Aerodynamic Design, Momentum Press, New York, NY, 2016. 276 pages.\u00a0<strong>ISBN-13:<\/strong>\u00a0978-1606509456<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-438\" src=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/11\/RaES-Awards-2025-500x355.jpg\" alt=\"\" width=\"500\" height=\"355\" srcset=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/11\/RaES-Awards-2025-500x355.jpg 500w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/11\/RaES-Awards-2025-1000x710.jpg 1000w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/11\/RaES-Awards-2025.jpg 1446w\" sizes=\"auto, (max-width: 500px) 100vw, 500px\" \/><\/p>\n<p><strong>Traditional Journal Articles<\/strong><\/p>\n<ol>\n<li><strong>Takahashi, T.T.,<\/strong> &#8220;On the Impact of Dispatch Weight Restrictions on Derivative Aircraft Propulsion Technology Evaluation,&#8221; MDPI Aerospace (in press), 2026.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Development of Improved Empirical Landing Equations for Conceptual Design,&#8221; MDPI Aerospace, Vol 13, No.4, p. 390, 2026. <a href=\"https:\/\/doi.org\/10.3390\/aerospace13040390\">https:\/\/doi.org\/10.3390\/aerospace13040390<\/a><\/li>\n<li><strong>Takahashi, T.T., <\/strong>Camberos, J.A., and Grandhi, R.V., &#8220;Design Limitations for Runway Operations of Gliding Aircraft,&#8221; AIAA Journal of Aircraft, 2025.\u00a0 <a href=\"https:\/\/arc.aiaa.org\/doi\/10.2514\/1.C038617\">https:\/\/arc.aiaa.org\/doi\/10.2514\/1.C038617<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Development of Improved Empirical Take-Off Equations,&#8221; MDPI Aerospace, Vol. 12, 2025. <a href=\"https:\/\/doi.org\/10.3390\/aerospace12080695\">https:\/\/doi.org\/10.3390\/aerospace12080695<\/a><\/li>\n<li>Lorenzo, W.P., Grandhi, R.V., and <strong>Takahashi, T.T.<\/strong>, &#8220;Investigation of Stability and Control Shortcomings of the North American X-15,&#8221; MDPI Aerospace, Vol. 12, 2025. <a href=\"https:\/\/doi.org\/10.3390\/aerospace12060513\">https:\/\/doi.org\/10.3390\/aerospace12060513<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Lorenzo, W.P., \u201cGoose Didn\u2019t Have to Die: The Evolution of Lateral\/Directional Departure Metrics and the Design of the F-14A,\u201d Royal Aeronautical Society Journal of Aeronautical History, 2025-04, pp. 1-58, 2025.<a href=\"https:\/\/www.aerosociety.com\/publications\/jah-goose-didn-t-have-to-die-the-evolution-of-lateraldirectional-departure-metrics-and-the-design-of-the-f-14a\">https:\/\/www.aerosociety.com\/publications\/jah-goose-didn-t-have-to-die-the-evolution-of-lateraldirectional-departure-metrics-and-the-design-of-the-f-14a<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Griffin, J.A. and Grandhi, R.V., \u201cHigh-Speed Aircraft Stability and Control Metrics,\u201d MDPI Aerospace, Vol. 12, 2025. <a href=\"https:\/\/doi.org\/10.3390\/aerospace12010012\">https:\/\/doi.org\/10.3390\/aerospace12010012<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cEzra Kotcher: the Father of the Bell X-1 and X-2,\u201d Royal Aeronautical Society Journal of Aeronautical History, 2024-04, pp. 73-143, Oct. 2024. <a href=\"https:\/\/www.aerosociety.com\/publications\/jah-ezra-kotcher-the-father-of-the-bell-x-1-and-x-2\/\">https:\/\/www.aerosociety.com\/publications\/jah-ezra-kotcher-the-father-of-the-bell-x-1-and-x-2\/<\/a> (winner of the 2024 RaES Journal of Aeronautical History Best Paper prize)<\/li>\n<li>McDonald, R.A., German, B.J, <strong>Takahashi, T.T.<\/strong>, Bil, C., Anemaat, W., Chaput, A., Vos, R. and Harrison, N., \u201cFuture Aircraft Concepts and Design Methods,\u201d Royal Aeronautical Society Aeronautical Journal, p. 1-33, Jan 2022. (2022 winner of a RAeS &#8220;Bronze&#8221; award for best written paper)<\/li>\n<li><strong> Takahashi, T.T.<\/strong>, \u201cThe Rise of the Drones \u2013 A Need for the Comprehensive Federal Regulation of Robot Aircraft,\u201d Albany Government Law Review, Vol. 8, No. 1, 2015, pp. 63-128.\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Takahashi-RiseOfDrones-AlbanyLawReview-SSRN-id2266221.pdf\">Takahashi-RiseOfDrones-AlbanyLawReview-SSRN-id2266221<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cRegulatory Changes to Enable the Development of More Efficient Transport Category Aircraft,\u201d AIAA Journal of Aircraft, Vol. 50, No. 5, pp. 1353-1368, Sep-Oct 2013. (DOI: 10.2514\/1.C031633).<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cDrones and Privacy,\u201d Columbia Sci. &amp; Tech. Law Rev, Vol. XIV, No. 1, Fall 2012, pp. 72-114.\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/DronesAndPrivacy-PrePrint-SSRN-id2035575.pdf\">DronesAndPrivacy-PrePrint-SSRN-id2035575<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong><em>,<\/em> &#8220;Drones in the National Airspace,&#8221; SMU Journal of Air Law and Commerce, Vol. 77, No.3, Summer 2012, pp. 489-533. <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Drones-in-the-National-Airspace-JAirLawCommerce-2012.pdf\">Drones in the National Airspace-JAirLawCommerce-2012<\/a><\/li>\n<li><strong style=\"font-size: 1rem;\">Takahashi, T.T.<\/strong><span style=\"font-size: 1rem;\">, German, B.J., Shajanian, A., Daskilewicz, M., and Donovan, S. &#8220;Form Factor and Critical Mach Number Estimation for Finite Wings,&#8221; AIAA Journal of Aircraft, Vol. 49, No. 1, Jan-Feb 2012. (DOI:10.2514\/1.C031466).<\/span><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cOptimum Transverse Span Loading for Subsonic Transport Category Aircraft,\u201d AIAA Journal of Aircraft, Vol. 49, No. 1, Jan-Feb 2012. (DOI:10.2514\/1.C031512).<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cOptimum Aspect Ratio for Subsonic Air Vehicles,\u201d AIAA Journal of Aircraft, Vol.48, No. 6, Nov-Dec 2011, pp. 1984-1993.\u00a0 (DOI:10.2514\/1.C031402).<\/li>\n<li>Daskilewicz, M. J., German, B.J., <strong>Takahashi, T.T.<\/strong>, Donovan, S., and Shajanian, A., \u201cEffects of Disciplinary Uncertainty on Multi-Objective Optimization in Aircraft Conceptual Design,\u201d Structural and Multidisciplinary Optimization, Vol. 44, No. 6 (2011), pp. 831-846 (DOI:10.1007\/s00158-011-0673-4).<\/li>\n<li>Takahashi, T., Feely, R. A., Weiss, R., Wanninkhof, R. H., Chipman, D. W., Sutherland, S. C. and <strong>Takahashi, T. T.<\/strong>, &#8220;Global air-sea flux of CO<sub>2<\/sub>: an estimate based on measurements of sea-air pCO<sub>2<\/sub> difference,&#8221; Proc. Nat. Acad. Sci., vol. 94, 8292-8299, 1997.<\/li>\n<li>Takahashi, T., <strong>Takahashi, T. T.<\/strong> and Sutherland, S. C., &#8220;An Assessment Of The Role Of The North Atlantic as a CO<sub>2<\/sub> Sink,&#8221; Phil. Transactions Of The Royal Society Of London, Series B, Vol. 348, pp. 143-152, 1995.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Flow Beneath a Rotating Annulus,&#8221; Physics of Fluids, Vol. 6, No. 5, 1994, pp. 1677-83.<\/li>\n<li>Benson, R.C. and <strong>Takahashi, T.T.<\/strong>, &#8220;Mechanics of Flexible Disks in Magnetic Recording,&#8221; ASME Advances in Information Storage Systems, Vol. 1, No. 1, 1991, pp. 15-35.<\/li>\n<\/ol>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-323\" src=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/RAeS-Awards-1-500x333.jpg\" alt=\"\" width=\"500\" height=\"333\" srcset=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/RAeS-Awards-1-500x333.jpg 500w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/RAeS-Awards-1-1500x1000.jpg 1500w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/RAeS-Awards-1-1000x667.jpg 1000w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/RAeS-Awards-1-1536x1024.jpg 1536w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/RAeS-Awards-1.jpg 1800w\" sizes=\"auto, (max-width: 500px) 100vw, 500px\" \/><\/p>\n<p><strong>Peer Reviewed Conference Papers\u00a0 &#8211; Scholar.Google.Indexed<\/strong><\/p>\n<ol>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Gaydusek, B.S.<\/u>, \u201cRethinking the Flying Qualities of the Avro Canada CF-105, the First Stability Augmented Supersonic Fighter,\u201d Accepted Paper for AIAA Aviation 2026, 2026.<\/li>\n<li><u style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">Lorenzo, W.P.<\/u><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\"> and<strong> Takahashi, T.T.<\/strong>, \u201cInvestigation of Spin Susceptibility Requirements for High Speed Vehicles,\u201d Accepted Paper for AIAA Aviation 2026, 2026.<\/span><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Revisiting Roskam\u2019s Empirical Predictions for Takeoff &amp; Landing to Support MIL 3013 Multi-Engine Aircraft Design,&#8221; Accepted Paper for AIAA Aviation 2026, 2026.<\/li>\n<li><em>Beaty, A.<\/em> and <strong>Takahashi, T.T.<\/strong>, &#8220;Throttle Dependent Forces Associated with Sub-Critical and Super-Critical Flows Over Internally Diffusing Pitot Inlets,&#8221; Accepted Paper for AIAA Aviation 2026, 2026.<\/li>\n<li><em>Bryan, B.C<\/em>. and <strong>Takahashi, T.T.<\/strong>, &#8220;Exploring the High-Speed Controllability Limits of the Bell X-1E,&#8221; Accepted Paper for AIAA Aviation 2026, 2026.<\/li>\n<li><em>Nugent, J<\/em>. and <strong>Takahashi, T.T.<\/strong>, &#8220;High-Speed Aircraft Controllability due to High-Altitude Atmospheric Turbulence \u2013 A History,&#8221; Accepted Paper for AIAA Aviation 2026, 2026.<\/li>\n<li>Atchison, S., <strong>Takahashi, T.T.<\/strong> and Camberos, J.A. &#8220;Linking Stability &amp; Control and Trajectory Analysis Tools in a High-Speed Vehicle Conceptual Design Process,&#8221; Accepted Paper for AIAA Aviation 2026, 2026.<\/li>\n<li><strong>Takahashi, T.T<\/strong>., \u201cDesign Challenges Faced by Actively Stabilized High Performance Aircraft,\u201d<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/07\/T-DesignChallengesActivelyStabilizedHighSpeedAircraft-AIAA-2025-3222.pdf\">AIAA-2025-3222<\/a>, 2025.<\/li>\n<li><u>Iyer, A.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cChallenges Quantifying the Transonic Characteristics of Swept Tuberculated Leading Edge Wings,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/07\/ArvindT-SweptTurberculatedWingPaper-AIAA-2025-3226.pdf\">AIAA-2025-3226<\/a>, 2025.<\/li>\n<li><strong>Takahashi, T.T<\/strong>. and <u>Lorenzo, W.P.<\/u>, \u201cThe Effect of Lateral\/Directional Departure Metrics on the Design of the F-14A,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2025\/07\/LateralDirectionalDesignMetricsF14-AIAA-2025-3115.pdf\">AIAA-2025-3115<\/a>, 2025.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, <u>Lorenzo, W.P.<\/u>, <u>Gaydusek, B.S.<\/u> and <u>Griffin, J.A.<\/u>, \u201cVORLAX 2024: Further Upgrades to a Legacy Potential Flow Solver,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/12\/AIAA-2025-0848-VORLAX2024.pdf\">AIAA-2025-0848<\/a>, 2025<\/li>\n<li><u>Iyer, A.G.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cReexamining Busemann\u2019s Wing Sweep Theory \u2013 A Modern Explanation of Classic Wartime Test Results,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/12\/AIAA-2025-2622-ArvindT-WingSweep.pdf\">AIAA-2025-2622<\/a>, 2025.<\/li>\n<li><u>Bryan, B.C.<\/u>, <u>Weissman, E.M.<\/u>, <u>Phung, J.V.<\/u>, <u>Jackson, Z.R.<\/u>, <u>Leo, J.D.<\/u>, <u>Stonemetz, J.E.<\/u>, <u>Caterial, W.G.<\/u>, <u>Hadimani, E.<\/u>, <u>Cana, L.J.<\/u>, <u>Cea, J.A.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cAerodynamic Design of an Executive Transport Optimized for Flight Just Beyond Mach One,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/12\/AIAA-2025-1048-NearSonicBusinessJet.pdf\">AIAA-2025-1048<\/a>, 2025.<\/li>\n<li><u>Kulkarni, A.S.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cOn the Design Implications of Elliptical and Bell-Shaped Lift Distributions,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/12\/AIAA-2025-2622-AmoghT.pdf\">AIAA-2025-2622<\/a>, 2025.<\/li>\n<li><strong>Takahashi, T.T,<\/strong> \u201cClimb Performance of Very High T\/W airframes,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-3194-ClimbAtHighTW.pdf\">AIAA-2024-3194<\/a>, 2024.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Camberos, J.A. and Grandhi, R.V., \u201cLanding Field Performance of Low L\/D Gliding Airframes,\u201d\u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-3911-LowLDLanding-final.pdf\">AIAA-2024-3911<\/a>, 2024.<\/li>\n<li><strong>Takahashi, T.T.,<\/strong> \u201cEzra Kotcher and the Configuration Aerodynamics of the Bell X-1 and X-2,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-4136-KotcherX1X2.pdf\">AIAA-2024-4136<\/a>, 2024.<\/li>\n<li><strong>Takahashi, T.T.,<\/strong> \u201cStandby Rocket Systems to Facilitate Noise Abatement of Future Commercial Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-3912-RocketAssistTO.pdf\">AIAA-2024-3912<\/a>, 2024.<\/li>\n<li><u>Uribe-Quintero, E.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cFlight Dynamics Issues of Control Coupling \/ Inertia Coupling Prone High-Speed Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-4048-EvT-WeissmanPaper-Aviation2024-final.pdf\">AIAA-2024-4048<\/a>\u00a0, 2024.<\/li>\n<li><u>Lorenzo, W.P.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cA Reassessment of the Controllable Flight Envelope of the Bell X-1A Rocket Plane,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-4138-WillT-BellX1A-Aviation2024.pdf\">AIAA-2024-4138<\/a>,\u00a0 2024.<\/li>\n<li><u>Garcia, J.<\/u>, <u>Asparuhov, B.<\/u>, <u>Stuck, S.<\/u>, <u>Bocek, J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cChallenges Designing Bio-Ethanol Fueled Airliners for Sustainable Intercontinental Aviation,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-3748-BioEthanolAircraft-Aviation2024.pdf\">AIAA-2024-3748<\/a>, 2024.<\/li>\n<li><u>Iyer, A.<\/u>, and <strong>Takahashi, T.T<\/strong>., \u201cThe Impact of Drop-In vs. Dedicated Sustainable Aviation Fuel on Aircraft Performance and Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-3986-ArvindT-SustainableAviationFuel.pdf\">AIAA-2024-3986<\/a>\u00a0, 2024.<\/li>\n<li><u style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">Uribe-Quintero, E.<\/u><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">, <\/span><u style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">Moreno, A.<\/u><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">, <\/span><u style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">Lehmbeck, T.<\/u><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">, <\/span><u style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">Anderson, S.<\/u><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\"> and <strong>Takahashi, T.T<\/strong>., \u201cA Technical Study Demonstrating the Poor Marketability of Near-Sonic Ultra-Long-Haul-Range Airliners,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/07\/AIAA-2024-4321-MarketabilityOfNearSonicAirliner.pdf\">AIAA-2024-4321<\/a>, 2024.<\/span><\/li>\n<li><strong style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">Takahashi, T.T.<\/strong><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">, \u201cNoise and Field Performance Impacts of FADEC Speed Scheduled Thrust Derate,\u201d <\/span><a style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\" href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-1705-1.pdf\">AIAA-2024-1705<\/a><span style=\"background-color: var(--bs-body-bg); font-size: var(--bs-body-font-size); text-align: var(--bs-body-text-align);\">, 2024.<\/span><\/li>\n<li><em>Hoopes, C.S,<\/em> and <strong>Takahashi, T.T.<\/strong>, \u201cLateral-Directional Controllability Impacts of Longitudinal Pitch Trim Strategies on the Space Shuttle Orbiter,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2318.pdf\">AIAA-2024-2318<\/a>, 2024.<\/li>\n<li><em style=\"font-size: revert;\">Heinz, J.H.<\/em><span style=\"font-size: revert;\"> and <strong>Takahashi, T.T.<\/strong>, \u201cAttainable Moment Sets \u2013 Approaches to Understanding Trim Capability in Conceptual Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2319.pdf\">AIAA-2024-2319<\/a>, 2024.<\/span><\/li>\n<li><span style=\"font-size: revert;\"><em>O\u2019Brien, K.P.<\/em> and <strong>Takahashi, T.T.<\/strong>, \u201cTail Sizing Strategies to Ensure Low-Risk Maneuvering High-Speed Flight,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2320.pdf\">AIAA-2024-2320<\/a>, 2024.<\/span><\/li>\n<li><span style=\"font-size: revert;\"><em>DeRoo, M.<\/em> and <strong>Takahashi, T.T<\/strong>., \u201cA Study of the Economic Viability of Commercial Supersonic Flight,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2214.pdf\">AIAA-2024-2214<\/a>, 2024.<\/span><\/li>\n<li><span style=\"font-size: revert;\"><em>Lorenzo, W.P.<\/em> and <strong>Takahashi, T.T.<\/strong>, \u201cReconstructing and Reassessing Neil Armstrong\u2019s \u201cFirst Man\u201d Flight in the North American X-15,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2643.pdf\">AIAA-2024-2643<\/a>, 2024.<\/span><\/li>\n<li><span style=\"font-size: revert;\"><em>Lorenzo, W.P.<\/em> and <strong>Takahashi, T.T.<\/strong>, \u201cCan We Fly it? Yes, We Can: A Comparative Study of Military Airworthiness and Flight Operations,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2213.pdf\">AIAA-2024-2213<\/a>, 2024.<\/span><\/li>\n<li><span style=\"font-size: revert;\"><strong>Takahashi, T.T<\/strong>., Camberos, J. and Grandhi, R.V., \u201cDetermination of Optimal Cruise Points for General Purpose Hypersonic Airframes,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2117.pdf\">AIAA-2024-2117<\/a> ,\u00a0 2024.<\/span><\/li>\n<li><span style=\"font-size: revert;\"><em>Valenzuela, J.V.<\/em> and <strong>Takahashi, T.T.<\/strong>, \u201cWing Design Strategies for Vehicles Designed to Operate in Ground Effect,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-0003.pdf\">AIAA-2024-0003,<\/a>\u00a02024.<\/span><\/li>\n<li><em>Puentes, O.G.<\/em> and <strong>Takahashi, T.T.<\/strong>, \u201cWingtip Treatments for Transonic Wing Planforms,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-0001.pdf\">AIAA-2024-0001<\/a>, 2024.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, <em>Griffin, J.A.<\/em> and Grandhi, R.V., &#8220;A Review of High-Speed Aircraft Stability and Control Challenges,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-3231-TGriffinGrandhi-HighSpeedSC-final-approved.pdf\">AIAA-2023-3231<\/a>,2023.\u00a0 Also issued as USAF contractor report AFRL-RQ-WP-TR-2022-0082, Aug. 2022 (available at https:\/\/apps.dtic.mil\/sti\/trecms\/pdf\/AD1195318.pdf)<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Lichtenstein, G.L., &#8220;Introducing the \u201cEntrepreneurial Mindset\u201d into Arizona State University\u2019s Aerospace Engineering Capstone Design,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-3661-KEEN-Capstone.pdf\">AIAA-2023-3661<\/a>,2023.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Whither Gander? A Business Case to Revive a Northern Hub Airport to Reduce Transatlantic Emissions,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-4302-Gander.pdf\">AIAA-2023-4302<\/a>,2023.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Flying with Eyes Wide Shut &#8211; A Reflection on the Hollywood View of Real World Aircraft Performance,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-3518-TopGunCommentary-final-final.pdf\">AIAA-2023-3518<\/a>\u00a0,2023.<\/li>\n<li><em>O&#8217;Brien, K.P.<\/em> and <strong>Takahashi, T.T.<\/strong>, &#8220;Configuration and Control Strategies for Maneuvering Supersonic Flight,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-3233-OBrienT-SalvagingTheX-2.pdf\">AIAA-2023-3233<\/a>,2023.<\/li>\n<li><em>Hoopes, C.S.<\/em> and <strong>Takahashi, T.T.<\/strong>, &#8220;A Study of High Speed Aerodynamic Configurations Optimized for Lateral-Directional Controllability,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-3235-HoopesT-HighSpeedLateralDirectional.pdf\">AIAA-2023-3235<\/a>, 2023.<\/li>\n<li><em>Ratnayake, S.S.<\/em> and <strong>Takahashi, T.T.<\/strong>, &#8220;Low Aspect Ratio High-Lift Wing Design for Automotive Racing Applications,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2023-4311-SajT-Formula1FrontWingDesignPaper-final3.1.pdf\">AIAA-2023-4311<\/a>,2023.<\/li>\n<li><strong>Takahashi, T.T<\/strong>., \u201cManeuvering Capabilities of Hypersonic Airframes,\u201d\u00a0 \u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/ManeuveringCapabilityHypersonic-AIAA-SciTech2023-final.pdf\">AIAA-2023-2247<\/a>, 2023.<\/li>\n<li><u style=\"font-size: 1rem;\">Heinz, J.H.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">O\u2019Brien, K.P.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Kosednar, D.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Hatch, T.<\/u><span style=\"font-size: 1rem;\"> and <strong>Takahashi, T.T.,<\/strong> \u201cSky Cruiser \u2013 A Design Study in Space Tourism \u201c, <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/SkyCruiser_AIAA_SciTech2023-final.pdf\">AIAA-2023-1355<\/a>, 2023<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2024\/01\/AIAA-2024-2643.pdf\">AIAA-2024-2643<\/a><\/span><\/li>\n<li><u style=\"font-size: 1rem;\">Stauffer, M.T.<\/u><span style=\"font-size: 1rem;\"> and <strong>Takahashi, T.T.<\/strong>, \u201cA History and Commentary on Thrust\/Drag Bookkeeping,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/StaufferT-ForceAccounting-AIAASciTech2023-final.pdf\">AIAA-2023-1553<\/a>, 2023.<\/span><\/li>\n<li><u>Hoopes, C.S.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cDevelopments in the Federal Regulation of Personal Air Vehicle,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/ConnorT-PAV-CFR-Requirements-Limitations-AIAA-SciTech2023-final.pdf\">AIAA-2023-0177<\/a>, 2023.<\/li>\n<li><u>Griffin, J.A.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cA Break from Tradition: The \u201cNew\u201d 14 C.F.R. Part 23 and Consensus Standards,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/GriffinT-BreakFromTraditionPart23-final.pdf\">AIAA 2023-0116<\/a>, 2023.<\/li>\n<li><u>Griffin, J.A.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cHypersonic Aircraft Performance Limitations Arising from Aerodynamic Control Limits,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/TakahashiGriffin-MissionSC-SciTech2023-final.pdf\">AIAA-2023-2248<\/a>, 2023.<\/li>\n<li><u style=\"font-size: 1rem;\">Griffin, J.A., <\/u><span style=\"font-size: 1rem;\"><strong>Takahashi, T.T.<\/strong> and Rodi, P.E., \u201cAerothermodynamic Assessment of Conceptual and Detail Configuration Changes to a Rocket Propelled Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/TakahashiGriffin-MissionThermalTrades-SciTech2023-final.pdf\">AIAA-2023-0216<\/a>, 2023.<\/span><\/li>\n<li><u>Stauffer, M.T., Backlund, M., Gonzales, Z.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cMulti-Disciplinary Design of an LH2 Powered Regional Jet\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Max_Capstone_SciTech2023_penultimate.pdf\">AIAA-2023-0980<\/a>, 2023<\/li>\n<li><strong>Takahashi, T.T<\/strong>., \u201cManeuvering Capabilities of High Payload Fraction Airframes,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/ManeuveringCapability-AIAA-Aviation2022-final.pdf\">AIAA-2022-3655<\/a>, 2022.<\/li>\n<li><u>Martinez-Rodriguez, G.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cRapid Design of a High-Lift Wing using Potential Flow Methods,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2022-3584.pdf\">AIAA-2022-3584<\/a>, 2022.<\/li>\n<li><u style=\"font-size: 1rem;\">Blair, M.<\/u><span style=\"font-size: 1rem;\"> and <\/span><strong style=\"font-size: 1rem;\">Takahashi, T.T<\/strong><span style=\"font-size: 1rem;\">., \u201cOptimal Composite Structural Design of Unmanned Aerial System Wings,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2022-4009.pdf\">AIAA-2022-4009<\/a>, 2022.<\/span><\/li>\n<li><u>Griffin, J. A.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cAero-Spaceplane Mission Performance Estimations Incorporating Atmospheric Control Limits,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/GriffinTakahashi-MissionSC-Aviation2022-finalissimo2.pdf\">AIAA-2022-3656<\/a>, 2022.<\/li>\n<li><u>Webb, B.D.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cAn Investigation of Static Aeroelastic Effects on Aircraft Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/BenT-aeroelasticdesign-AIAA-Aviation2022-final.pdf\">AIAA-2022-3587<\/a>, 2022.<\/li>\n<li><u>Griffin, J. A.<\/u> , <strong>Takahashi, T.T.<\/strong> and Rodi, P.E., \u201cAerothermodynamic Modeling for a \u201cMission Code\u201d Approach to Hypersonic Flight,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/JackTR-MissionThermal_AIAA-Aviation_finalissimo2.pdf\">AIAA-2022-3657<\/a>, 2022.<\/li>\n<li><u>O\u2019Brien, K.P. <\/u>and <strong>Takahashi, T.T.<\/strong>, \u201cAn Investigation of the Bell X-2 and the Factors that Led to Its Fatal Accident,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/OBrienT-BellX2-AIAA-Aviation2022-final.pdf\">AIAA-2022-3203<\/a>, 2022.<\/li>\n<li><u>Hoopes, C.<\/u>, <u>Chaidez, G.<\/u>, <u>Mulkern, W<\/u>, <u>Heitmann, K.<\/u>, <u>Olszak, P.<\/u>, <u>Ayoub, K.<\/u>, <u>Nagpal, P.<\/u>, <u>Raganathan, A. <\/u>and <strong>Takahashi, T.T.<\/strong>, \u201cDesign of a N+1 Feeder Aircraft for Regional Cargo Airlines,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Hoopes-CargoFeeder-AIAA-Aviation2022-final-final-final.pdf\">AIAA-2022-3377<\/a>, 2022.<\/li>\n<li><u>Chaudhari, B.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cReassessing the B2707-100 Supersonic Transport Aircraft,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/BhargavT-B2707-100-History-final-final.pdf\">AIAA-2022-0776<\/a>, 2022.<\/li>\n<li><u>Chaudhari, B.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cInlet Diffusor Buoyancy \u2013 Its Historical Use in Supersonic Transport Design,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2022-2566-InletDiffusorBuoyancy-1.pdf\">AIAA2022-2566<\/a>, 2022.<\/li>\n<li><u>Souders, T.J.<\/u>, <u>Heitmann, K.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cLife in the Fast Lane: Project-Based Learning of Advanced Aerodynamics Using a Rapid Potential Flow Code,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2022-1350-VORLAXusepaper-SoudersHeitmannTakahashi.pdf\">AIAA2022-1350<\/a>, 2022.<\/li>\n<li><u>Webb, B.D.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cEmerging Federal Regulatory Framework For Future Supersonic Transport Aircraft,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2022-0366-FederalRegofSST.pdf\">AIAA2022-0366<\/a>, 2022.<\/li>\n<li><u>Ratnayake, S.S.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cNew Approaches to Direct Wing Shape Synthesis using Potential Flow Solvers.\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2022-0547.pdf\">AIAA-2022-0547<\/a>, 2022.<\/li>\n<li><u>Armenta, F.X<\/u>., <u>Plaban, P.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cRevisiting Neumark\u2019s Critical Pressure Coefficient Rule for Aircraft with Finite Wings,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2022-1157-NeumarkRevisted-ArmentaPlabanTakahashi.pdf\">AIAA-2022-1157<\/a>, 2022.<\/li>\n<li><u>Martinez-Rodriguez, G.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cReflections On Using Potential Flow Codes to Design High-Lift Systems,\u201d\u00a0 \u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2022-1155-PotentialFlowHighLiftSystems-GabinoT.pdf\">AIAA-2022-1155<\/a>, 2022.<\/li>\n<li><strong>Takahashi, T.T.,<\/strong> \u201cEmpirical Methods to Predict Takeoff Field Requirements for Single-Engine Aircraft,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2022-0548-EmpiricalMethodsForSingleEngineTakeoff.pdf\">AIAA-2022-0548<\/a>, 2022.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cRevisiting Roskam\u2019s Empirical Predictions for Critical Field Length,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2446-RevisitRoskam1.pdf\">AIAA-2021-2446<\/a> , 2021.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cRevisiting Roskam\u2019s Empirical Predictions for Landing Distance,\u201d\u00a0 \u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2447-RevistRoskam2.pdf\">AIAA-2021-2447<\/a>, 2021.<\/li>\n<li><u>Souders, T.J.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cVORLAX 2020: Making a Potential Flow Solver Great Again,\u201d\u00a0 \u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2458-VORLAX2020-MakingSolverGreatAgain.pdf\">AIAA-2021-2458<\/a>, 2021.<\/li>\n<li><u>Souders, T.J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cVORLAX 2020: Benchmarking Examples of a Modernized Potential Flow Solver,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2459-VORLAX2020-Benchmarks.pdf\">AIAA-2021-2459<\/a>, 2021.<\/li>\n<li><u>Kurus, N.J.<\/u>, <strong>Takahashi, T.T.<\/strong> and Perez, R.E., \u201cCritical Mach Number Predictive Methods for Realistic Supersonic Wing \/ Body Configurations,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2432-NoahTRuben.pdf\">AIAA-2021-2432<\/a>, 2021.<\/li>\n<li><u>Armenta, F.X.<\/u> and <strong>Takahashi, T.T.<\/strong>,\u00a0 \u201cRevisiting the Transonic Area Rule for Conceptual Aerodynamic Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/FrankieT-WaveDrag-Aviation2021-Final.pdf\">AIAA-2021-2441<\/a>, 2021.<\/li>\n<li><u>Plaban, P.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cAerodynamic Design Challenges of a Thin Transonic Wing,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2423.pdf\">AIAA-2021-2423<\/a>, 2021.<\/li>\n<li><u>Frost, L.<\/u>, <u>Chia, V.<\/u>, <u>Reuland, J.<\/u>, <u>Namera, S.<\/u>, <u>Moreno, E.<\/u>, and <strong>Takahashi, T.T.,<\/strong> \u201cPreliminary Design of a Trans-Atlantic High Speed Civil Transport,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-2418-Luke-SST-1.pdf\">AIAA-2021-2418 <\/a>, 2021.<\/li>\n<li><u>Kurus, N.J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cAerodynamic Design of a Mach 1.3 Airliner,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/NoahT-SciTech2021paper-FINAL-FINAL.pdf\">AIAA-2021-0591<\/a>, 2021.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cDevelopment of a Semi-Empirical Takeoff &amp; Landing Method for Supersonic Aircraft,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/T-Supersonic-TOLD-AIAA-2021-0462-final.pdf\">AIAA-2021-0462<\/a>, 2021.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Perez, R.E., \u201cThe Assumed Wind Procedure to Increase Dispatch Safety for VMCA Limited Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/TPerez-AssumedWinds-SciTech2021-final.pdf\">AIAA-2021-0459<\/a>, 2021.<\/li>\n<li><u>Kurus, N.J.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cDoes Your Aircraft\u2019s Metabolism Slow with Time? : An Analysis of Flight Performance Degradation Associated with Aging Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/NoahT-AgingAircraftPerformanceLoss-final.pdf\">AIAA-2021-0460<\/a>, 2021.<\/li>\n<li><u>Schierbrock, A<\/u>. and <strong>Takahashi, T.T.,<\/strong> \u201cReconstruction of Flight-Path Dependent Aircraft Point-Performance, Stability &amp; Control from Public Flight Data,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-0325.pdf\">AIAA-2021-0325<\/a>, 2021.<\/li>\n<li><u>Martinez-Rodriguez, G.<\/u>, <u>Fratangelo, D.<\/u>, <u>Fregoso, E.I.<\/u>, <u>Kosloske, T.<\/u>, <u>Kurt, H.<\/u>, <u>Schierbrock, A.<\/u>, <u>Valderama, D.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cMulti-Disciplinary Design of a Mid-Range Commercial Transport Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-0011.pdf\">AIAA-2021-0011<\/a>, 2021.<\/li>\n<li><u>Ratnayake, S S.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cImproved Synthesis Method to Develop Conceptual Design Wing Lofts,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2021-0218.pdf\">AIAA-2021-0218<\/a>, 2021.<\/li>\n<li><strong>Takahashi, T.T<\/strong>. and <u>Thomas, P.R<\/u>., \u201cThe Aerodynamic Design of a High-Altitude Operational-Return Unmanned System for Atmospheric Science,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2020-2658-TakahashiThomas-HORUS.pdf\">AIAA-2020-2658<\/a>, 2020.<\/li>\n<li><u>Thomas, P.R<\/u>. and <strong>Takahashi, T.T.,<\/strong>\u00a0 \u201cAircraft Should Not Be Fair Weather Friends \u2013 Impact of Winds Aloft on Aircraft Operating Economics,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/FairWeatherFriends-Aviation2020-Final.pdf\">AIAA-2020-2636<\/a>, 2020.<\/li>\n<li><u>Thomas, P.R<\/u>. and <strong>Takahashi, T.T<\/strong>., \u201cHow to Soar Above the Competition \u2013 Design Strategies to Improve Airliner Operating Economics in Real Weather,\u201d<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/SoaringAboveCompetition_aviation2020-final.pdf\">AIAA-2020-2637<\/a>, 2020.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Perez, R.E., \u201cThe Effect of Manufacturing Variation on Aerodynamic Performance and Flight Safety,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/T-P-AIAA2020Aviation-WarpedWing-final.pdf\">AIAA-2020-2649<\/a>, 2020.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Cleary, S.C.<\/u>, \u201cInlet Diffusor Buoyancy &#8211; An Overlooked Term in the Thrust Equation,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2020-2642.pdf\">AIAA-2020-2642<\/a>, 2020.<\/li>\n<li><u>Kolesov, N.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cDesign and Validation of Buckling Dominated Wing Structure for Small Unmanned Aerial Systems\u201d AIAA 2020-2654, 2020.<\/li>\n<li><u style=\"font-size: 1rem;\">Vasconcelos, P.E.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Lam, Y.-F.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Allen, A<\/u><span style=\"font-size: 1rem;\">., <\/span><u style=\"font-size: 1rem;\">Rivera, E.<\/u><span style=\"font-size: 1rem;\"> and <strong>Takahashi, T.T.<\/strong>, \u201cMultidisciplinary Optimization of a Next-Generation Narrow Body Transport\u201d AIAA 2020-2628, 2020.<\/span><\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Perez, R.E., \u201cOn the Operational Implications of Traditional Design Rules for Minimum Controllable Airspeed,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2020-0749-TakahashiPerez.pdf\">AIAA-2020-0749<\/a>, 2020.<\/li>\n<li><u style=\"font-size: 1rem;\">Halversen, H.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Mitchell, R.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Spear, M.<\/u><span style=\"font-size: 1rem;\">, <\/span><u style=\"font-size: 1rem;\">Vo, B.<\/u><span style=\"font-size: 1rem;\"> and <strong>Takahashi, T.T.<\/strong>, \u201cOptimal Design of an N+1 Narrow-Body Transport Aircraft,\u201d AIAA 2020-0270, 2020.<\/span><\/li>\n<li><u>Frede, K.<\/u> and<strong> Takahashi, T.T<\/strong>., \u201cComputational Methods for the Preliminary Design of Engine-Nacelle Placement on Transonic Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2020-1956.pdf\">AIAA-2020-1956<\/a>, 2020.<\/li>\n<li><u style=\"font-size: 1rem;\">Thomas, P.R<\/u><span style=\"font-size: 1rem;\">. and <strong>Takahashi, T.T.<\/strong>, \u201cAircraft En-Route Performance Considering Winds-Aloft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Wind_Missions_PT_final_final.pdf\">AIAA-2020-0748<\/a>, 2020<\/span><\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Ou, C.-W.<\/u>, \u201cWhen Higher Fidelity Models Degrade Our Understanding of Induced Drag &#8211; The Tragedy of the Treffetz Plane Integral,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2020-0276.pdf\">AIAA-2020-0276<\/a>, 2020.<\/li>\n<li><u>Thomas, P.R<\/u>. and <strong>Takahashi, T.T.,<\/strong> \u201cThe Wild West of Aviation: An Overview of Unmanned Aircraft Systems Regulation in the United States,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2020-0646-PhilThomas-WildWestDronePolicy.pdf\">AIAA-2020-0646-<\/a>, 2021.<\/li>\n<li><u>Burgett, L.M.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cComparison of Vaneless Counter-Rotating Power Extraction Engines for UAV Propulsion,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2019-3016.pdf\">AIAA-2019-3016<\/a>, 2019<\/li>\n<li><u>Cullymore, K.<\/u>, <u>Hines, C.<\/u>, <u>Soldevilla, J.<\/u>, <u>Patrick, N.<\/u>, <u>Loo, C.<\/u>, and <strong>Takahashi, T.T<\/strong>., \u201cMulti-Disciplinary Optimization of a N+1 Technology Mid-Market Aircraft,\u201d AIAA 2019-2881, 2019<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Sobester, A., \u201cClimb Performance Anomalies in \u2018Real\u2019 Atmospheric Conditions,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/TakahashiSobesterAIAA-final-final.pdf\">AIAA-2019-3271<\/a>, 2019<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Thomas, P.R.<\/u>, \u201cWAT\u2019s Up with Using the Small-Angle Approximation to Estimated Climb Gradient Limited Departure Weights,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/WATsup-ProblemsOfTheWorkEnergyTheorem_final.pdf\">AIAA-2019-3273<\/a>, 2019<\/li>\n<li><u>Miskin, D.L.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cPreliminary Design of a Wing Considering Transonic Aerodynamic, Weight and Aeroelastic Behavior,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2019-3068.pdf\">AIAA-2019-3068<\/a>, 2019<\/li>\n<li><u>Delisle, M.<\/u> and<strong> Takahashi, T.T<\/strong>., \u201cWe Wonder Why We Wallow: Impacts of Trim Error on Speed and Flight Path Stability,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/MatT-SciTech2019-PhugoigalFlight_final.pdf\">AIAA-2019-0559<\/a>, 2019<\/li>\n<li><strong>Takahashi, T<\/strong>.<strong>T<\/strong>., \u201cA Bad Moon Rising: The Puzzling Inaccuracies of the Work-Energy Theorem in Aircraft Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2019-1305.pdf\">AIAA-2019-1305<\/a> , 2019<\/li>\n<li><u>Milosavljevic, I.<\/u>, <u>Nuber, B.<\/u>, <u>Swarm, G.<\/u>, <strong>Takahashi T.T.<\/strong>, et al. \u201cPreliminary Design of a Long Range, Fuel Efficient High Performance Business Jet,\u201d AIAA 2019-0555, 2019<\/li>\n<li><strong>Takahashi, T.T<\/strong>., <u>Boccieri, S.<\/u>, <u>Elvig, J.<\/u>, <u>McClure, N.<\/u>, <u>Oroz, J.<\/u>, <u>Spiller, K.<\/u> and <u>Zurfluh, K<\/u>, \u201cPuzzling Problems Configuring a Forward Swept Wing Transonic Aircraft,\u201d AIAA 2019-0813, 2019<\/li>\n<li><u>Leader, R.<\/u> and<strong> Takahashi, T.T<\/strong>., \u201cFrosty Weather: The Regulatory History of Aircraft Operations in Freezing Conditions,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Leader_Takahashi_final.pdf\">AIAA-2019-1958<\/a>, 2019<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Stone, N.<\/u>, \u201cAircraft Performance Impacts of Power and Bleed Air Extraction on a COTS Engine Powered UAS.\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Takahashi_Stone_UAV_power_final.pdf\">AIAA-2019-1309<\/a>, 2019<\/li>\n<li><u>Beard, J.E<\/u>. and <strong>Takahashi, T.T.<\/strong>, \u201cWind Accountability and Obstacle Clearance Limited Takeoff for Commercial Transport Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2018-3501.pdf\">AIAA-2018-3501<\/a>, 2018<\/li>\n<li><u>Delisle, M.<\/u>, <u>Morrow, M.H.<\/u>, <u>Ramirez, A.<\/u>, <u>Padilla, M.<\/u>, <u>Thach, S.<\/u>, <u>Elliott, S.<\/u>, <u>Miller, T.<\/u> and<strong> Takahashi, T.T<\/strong>., \u201cPreliminary Design of a Next Generation Super-Mid-Size Business Jet,\u201d AIAA 2018-3024, 2018<\/li>\n<li><strong>Takahashi, T.T<\/strong> and <u>Delisle, M.<\/u>, \u201c(Un)stabilized Approach &#8211; An Introduction to Dynamic Flight Conditions during Takeoff and Landing Climb,\u201d<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Takahashi_delisle_Unstabilized_Flight_AIAA-2018-3500.pdf\">AIAA-2018-3500<\/a>, 2018.<\/li>\n<li><u>Delisle, M.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cSpeed Stability and Obstacle Clearance During Engine Inoperative Takeoff,\u201d<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Takahashi_delisle_UnstableTakeoff_AIAA-2018-3502.pdf\">AIAA-2018-3502<\/a>, 2018.<\/li>\n<li><u>Delisle, M.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cFloating Home: Speed Stability and Inadvertent Stalls During a Balked Landing,\u201d<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Takahashi_delisle_UnstableLanding_AIAA-2018-3509.pdf\">AIAA-2018-3509<\/a>, 2018<\/li>\n<li><u>Cleary, S.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cThe Effects of Fixed Conical Spike Inlets on the Performance of Higher Bypass Ratio Engines,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2018-3836.pdf\">AIAA-2018-3836<\/a>, 2018<\/li>\n<li><u>Miskin, D.L.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cStochastic Modeling of Preliminary Wing Box Structural Design for Stiffness,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2018-4002.pdf\">AIAA-2018-4002<\/a>, 2018<\/li>\n<li><u>Kallas, D.<\/u>, <u>Brown, K.<\/u>,<u> Remsing, T.<\/u>, <u>Ingham, J.<\/u>, <u>Miskin, D.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cDesign of a Dual-Use Aerobatic Light Jet,\u201d AIAA 2018-2030, 2018<\/li>\n<li><u>Wood, D.L.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cThe Effect of Piloting Practices Upon Actual as Opposed to Scheduled Landing Field Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2018-1756.pdf\">AIAA-2018-1756<\/a>, 2018<\/li>\n<li><u>Wood, D.L.<\/u>, <u>Beard, J.E.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cReal Pilots Don&#8217;t Go Around: Discontinued Approach and Balked Landing Climb Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/TakahashiWoodBeard-RealPilotsDontGoAroundPaper-final-final.pdf\">AIAA-2018-1752<\/a>, 2018<\/li>\n<li><u>Beard, J.E.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201c(Un)controlled Flight Into Terrain: A History of Obstacle Clearance Regulations,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/ControlledFlightIntoTerrain_final_final.pdf\">AIAA-2018-1614<\/a>, 2018<\/li>\n<li><u>Wood, D.L.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cExtraordinary Care: A History of Flight Operations Rules for Common Carriers,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2018-1616-Wood-CommonCarrier.pdf\">AIAA2018-1616<\/a>, 2018<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, <u>Beard, J.E.<\/u> and <u>Wood, D.L.<\/u>, \u201cThe Human Factor: Accounting For \u201cOff Book\u201d Flight Speeds Within Implied Safety Margins,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2018-0284.pdf\">AIAA-2018-0284<\/a> , 2018<\/li>\n<li><u>Beard, J.E.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cOptimal Piloting Approaches For Obstacle Clearance Limited Standard Instrument Departures,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2018-0285.pdf\">AIAA2018-0285<\/a>, 2018<\/li>\n<li><u>Hadder, E.M.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cMinimum Control Speed Estimation for Conceptual Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2017-3764.pdf\">AIAA-2017-3764<\/a>, 2017<\/li>\n<li><u>Wilson, J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cThe Doghouse Plot: History, Construction Techniques and Application,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2017-3266.pdf\">AIAA-2017-3266<\/a>, 2017<\/li>\n<li><u>Beard, J.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cRevisiting Takeoff Obstacle Clearance Procedures: An Argument for Extended Second Segment Climb,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2017-3265.pdf\">AIAA-2017-3265<\/a>, 2017<\/li>\n<li><u>Anderson, B.K.<\/u> and <strong>Takahashi, T.T<\/strong>., \u201cConceptual Fuselage Design with Direct CAD Modelling,\u201d AIAA 2017-3940, 2017<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, <em>D.<\/em><u>L. Wood<\/u> and Bays, L.V., \u201cThe Effect of Aerodynamic and Propulsive Uncertainty Upon Certified Takeoff Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2017-3420.pdf\">AIAA-2017-3420<\/a>, 2017<\/li>\n<li><u>Wood, D.L.<\/u>, <strong>Takahashi, T.T.,<\/strong> and Bays, L.V., \u201cExperimental Investigation of Typical Aircraft Field Performance versus Predicted Performance Targets,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2017-3276.pdf\">AIAA-2017-3276<\/a>, 2017<\/li>\n<li><u>Wood, D.L.<\/u>, <strong>Takahashi, T.T.,<\/strong> and Bays, L.V. \u201cThe Effect of Piloting Practices Upon Actual as Opposed to Scheduled Takeoff Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA2017-3422.pdf\">AIAA2017-3422<\/a>, 2017<\/li>\n<li><u>Wilson, J.<\/u>, <u>Teves, R.<\/u>, <u>Snodgrass, N.<\/u>, <u>Haley, J.<\/u>, and <strong>Takahashi, T.T.<\/strong>, \u201cMultidisciplinary Design Process for a 100 seat Regional Jet,\u201d AIAA 2017-3586, 2017.<\/li>\n<li><u>Verbin, A.J.<\/u>, <strong>Takahashi, T.T.<\/strong>, and White, D.B. \u201cDetail Design of a Pulsed Plasma Test Stand,\u201d AIAA 2017-4523, 2017.<\/li>\n<li><strong>Takahashi, T.T.,<\/strong> <u>Wood, D.L.<\/u> and Bays, L.V., \u201cAn Introduction to the Impact of Pilot Techniques Upon \u201cCertified\u201d Field Performance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2017-0007-TakahashiWoodBays-FieldPerformance.pdf\">AIAA-2017-0007<\/a>, 2017.<\/li>\n<li><u>Kirkman, J.J.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cCritical Mach Number Prediction on Swept Wings,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2017-0266-KirkmanTakahashi-CriticalMachNumberPredictionOnSweptWings.pdf\">AIAA-2017-0266<\/a>, 2017.<\/li>\n<li><strong>Takahashi, T.T.,<\/strong> <u>Kirkman, J.J.<\/u>, <u>Verbin, A.J.<\/u> and Cotting, M.C., \u201cAn Innovative Total-Flight-Envelope Approach to Teach Configuration Aerodynamics,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2017-0692.pdf\">AIAA-2017-0692<\/a>, 2017.<\/li>\n<li><u>Matthieu, M.S.<\/u>, <u>Marin, A.M.<\/u>, <u>Stephenson, K.J.<\/u>, <u>Beard, J.E.<\/u>, <u>Castillo, E.<\/u>, <u>Weddle-Weaver, C.<\/u>, <u>Teni, D.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cPreliminary Design of an N+1 Overwater Supersonic Commercial Transport Aircraft,\u201d .\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2017-1387-ScotteKyleJohn-SupersonicTransport.pdf\">AIAA-2017-1387<\/a>, 2017.<\/li>\n<li><u>Garnica, I.<\/u> and<strong> Takahashi, T.T.<\/strong>, \u201cA Study of Engine Parameters and Shaft Configuration on Transport Aircraft Performance,\u201d AIAA 2017-1854, 2017.<\/li>\n<li><u>Benassi, M.S.<\/u>, <u>Hrdina, C.R.<\/u>, <u>Horton, E.<\/u>, <u>Hadder, E.<\/u> and T<strong>akahashi, T.T.<\/strong> \u201cNext-Generation Regional Jet Transport Conceptual Design,\u201d AIAA 2017-1855, 2017.<\/li>\n<li><strong>Takahashi, T.T<\/strong>. and Bays, L.V., \u201cClimbing While Turning: Combat Energy Management Principles Applied to Civilian Obstacle Clearance,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2016-4217.pdf\">AIAA-2016-4217<\/a>, 2016.<\/li>\n<li><u>Palma, R.M.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cThe Effects of Supersonic Inlet Topology on the Installed Performance of Turbofan Engines,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2016-3463.pdf\">AIAA-2016-3463<\/a>, 2016.<\/li>\n<li><u>Allyn, M.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cConceptualizing Active-Load-Alleviation: Impacts on Transport Category Aircraft Wing Structural Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2016-3744.pdf\">AIAA-2016-3744<\/a>, 2016.<\/li>\n<li><u>Kirkman, J.J.<\/u> and\u00a0<strong>Takahashi, T.T.<\/strong>, \u201cRevisiting the Transonic Similarity Rule: Critical Mach Number Prediction Using Potential Flow Solutions,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2016-4329-KirkmanTakahashi-TransonicSimilarityRule.pdf\">AIAA2016-4329<\/a><u>, 2016.<\/u><\/li>\n<li><u>Jensen, J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cWing Design Challenges Explained: A Study of the Finite Wing Effects of Camber, Thickness, and Twist,\u201d\u00a0 \u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2016-0781-Takahashi-Jensen.pdf\">AIAA 2016-0781<\/a><u>, 2016<\/u><\/li>\n<li><u>Dickman, C.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cEngine\/Inlet Matching for Supersonic Aircraft Design,\u201d AIAA 2016-0771, 2016.<\/li>\n<li><u>Smith, D.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cImproved Field Performance through Regulatory Changes to Enable Speed Scheduled Reverse Thrust,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2016-1280.pdf\">AIAA-2016-1280<\/a>, 2016.<\/li>\n<li><u>Merrell, M.Q.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cRediscovering the Peakey Leading Edge: A Study of the Transonic Properties of Classic Airfoils,\u201d AIAA 2016-1564, 2016.<\/li>\n<li><u>Barchfeld<\/u><u>, C.A.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cBeyond the Elliptical Span Load: Optimizing Minimum Induced Drag Using Enhanced Leading Edge Suction,\u201d AIAA 2016-0781, 2016<\/li>\n<li><u>Kirkman, J.<\/u>, <u>Wood, D.<\/u>, <u> T.<\/u>, <u>Gurczak, M.<\/u>, <u>Rothlisberger, C.<\/u>, <u>Pan, K.Z.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cDesign Study for a Highly Fuel Efficient Regional Transport,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2016-1029.pdf\">AIAA-2016-1029<\/a>, 2016.<\/li>\n<li><u>Palma, R.M.<\/u>, <u>Thomas, M.E.<\/u>, <u>Balasiu, A.C.<\/u>, <u>Takamatsu, L.N.<\/u>, <u>Noonan, W.N.<\/u>, and <strong>Takahashi, T.T.<\/strong>, \u201cA Multi-Disciplinary Study of Future Fuel Efficient Regional Aircraft,\u201d AIAA 2016-1424, 2016.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Lemonds, T.<\/u>, \u201cPrediction of Wing Structural Mass for Transport Category Aircraft Conceptual Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2015-3374.pdf\">AIAA-2015-3374<\/a>, 2015.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cThe Impact of ATTCS on Reduced Thrust Takeoff Field Performance, <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA2015-2698.pdf\">AIAA-2015-2698<\/a>, 2015.<\/li>\n<li><strong>Takahashi, T.T<\/strong>., \u201cOptimal Climb Trajectories Through Explicit Simulation,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2015-2701-OptimalTrajectoryExplicitSimulation.pdf\">AIAA-2015-2701<\/a> , 2015.<\/li>\n<li><u>Mirochnitchenko, V.<\/u> and<strong> Takahashi, T.T.<\/strong>, \u201cAn Investigation into the Design of an Efficient In-Ground-Effect Flying Vehicle Platform, AIAA 2015-3000, 2015.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Kamat, S<\/u>., \u201cRevisiting Busemann: The Design Implications of Inconsistencies Found Within Simple Sweep Theory,\u201d AIAA 2015-3376, 2015.<\/li>\n<li><u>Swann, M.<\/u> and <strong>Takahashi, T.T.,<\/strong> \u201cA Total Flight Envelope Approach to Conceptual Design Stability &amp; Control,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2015-3377.pdf\">AIAA-2015-3377<\/a>, 2015.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Gedeon, C.<\/u>, \u201cThe Effect of Propulsion System Scale and Bypass Ratio Upon Optimum Climb Speed,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2015-1677.pdf\">AIAA-2015-1677<\/a>, 2015.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Lemonds, T.<\/u>, \u201cTransport Category Wing Weight Estimation Using A Optimizing Beam-Element Structural Formulation,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2015-1898.pdf\">AIAA-2015-1898<\/a>, 2015.<\/li>\n<li><u>Dulin, D.J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cDesign Implications of Elliptical Planform Wings,\u201d<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/06\/AIAA-2015-0397-EllipticalWings-DulinTakahashi.pdf\">AIAA-2015-0397<\/a>, 2015.<\/li>\n<li><u>Mirochnitchenko, V.<\/u>, <u>Swann, M.<\/u>, <u>Stallings, D.<\/u>,<u> Merrell, M.<\/u>, <u>Miller, D.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cMulti-Disciplinary Optimization of a Near Sonic Airliner,\u201d AIAA 2015-0132, 2015.<\/li>\n<li><u>Langley, C.<\/u>, <u>Burt, R.<\/u>, <u>Patel, N.<\/u>, <u>Martinez, I.<\/u>, <u>Leon, A.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cConceptual Design of a Mach 0.95 Cruise N+1 Commercial Transport,\u201d AIAA 2015-1901, 2015.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Kady, C.T.<\/u>, \u201cPlanform Selection for an Efficient Supersonic Air Vehicle,\u201d AIAA 2014-2426, 2014.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Creighton, A.<\/u>, \u201cReforming Field Performance Federal Aviation Regulations for Operational Safety and Consistency,\u201d AIAA 2014-2425, 2014.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, <u>Dulin, D.J.<\/u> and <u>Kady, C.T.<\/u>, \u201cA Method to Allocate Camber, Thickness and Incidence on a Swept Wing,\u201d AIAA 2014-3172, 2014.<\/li>\n<li><u>Gedeon, C.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cA Multi-Disciplinary Survey of Energy Maneuverability for Subsonic Endurance Based Aircraft,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2014-3156.pdf\">AIAA-2014-3156<\/a>, 2014.<\/li>\n<li><u>Gedeon, C.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cMulti-Disciplinary Survey of Engine Parameters and the Resulting Impact on Energy Maneuverability,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2014-2032.pdf\">AIAA-2014-2032<\/a>, 2014.<\/li>\n<li><u>Gibson, G.S.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cMulti-Disciplinary Design of a Rocket Engine Thrust Augmentation Ejector for Endoatmospheric Flight,\u201d AIAA 2014-3091, 2014.<\/li>\n<li><u>Heitzman, N.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cComparison of Commercial Flight Fuel Reserves in Regards to FAR, Numerical Simulation, and Pilot Flight Techniques,\u201d AIAA 2014-3263, 2014.<\/li>\n<li><u>Bowerman, K.<\/u>, <u>Chandran, P.<\/u>, <u>Ixtabalan, D.<\/u>, <u>Sheets, D.T<\/u>. and <strong>Takahashi, T.T.<\/strong>, \u201cA Systems Approach to Aircraft Synthesis and Optimization of a Light Business Aircraft,\u201d AIAA 2014-2854, 2014.<\/li>\n<li><u>Kady, C.T.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cAllocating Section Thickness and Camber for Transonic Wing Design,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/05\/AIAA-2014-0024.pdf\">AIAA-2014-0024<\/a>, 2014.<\/li>\n<li><u>Mora, N.<\/u>, <u>Heitzman, N.<\/u>, <u>Scoville, S.<\/u>, and <strong>Takahashi, T.T.<\/strong>, \u201cConceptual Design of a N+1 Transonic Executive Jet,\u201d AIAA 2014-0030, 2014.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cThe Public Domain, The National Interest and The Fate of the NASA Technical Reports Server,\u201d AIAA 2014-0281, 2014. Revised manuscript under the same title also available at: <a href=\"http:\/\/dx.doi.org\/10.2139\/ssrn.2425190\">http:\/\/dx.doi.org\/10.2139\/ssrn.2425190<\/a><\/li>\n<li><u>DeStories, J.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cFixed Pitch Propeller Design for Electrically Powered Aircraft,\u201d AIAA 2014-0537, 2014.<\/li>\n<li><u>Lyddon, J.<\/u>, <u>Nguyen, M.<\/u>, <u>Quackenbush, J.<\/u>, <u>Schadegg, T.<\/u> and <strong>Takahashi, T.T.<\/strong>, \u201cOptimum Design of a Fuel Efficient Mid-Size Business Jet,\u201d AIAA 2014-1337, 2014.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cIntellectual Property Law and Legacy FORTRAN Code,\u201d AIAA 2013-4210, 2013.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and <u>Kady, C.T.<\/u>, \u201cCurious Circumstances Surrounding Optimal Non-Planar Wings,\u201d AIAA 2013-4203, 2013.<\/li>\n<li><u>Gedeon, C.<\/u>, <u>Huffer, S.<\/u>, and <strong>Takahashi, T.T.<\/strong>, \u201cMulti-Disciplinary Design of an Advanced Narrow-Body Transport Aircraft,\u201d AIAA 2013-4329, 2013.<\/li>\n<li><u>Reed, T.<\/u>, <u>Jaksa, M.<\/u>, <u>Gomez, J.<\/u>, and <strong>Takahashi, T.T.<\/strong>, \u201cHigh Altitude Hot Rod \u2013 An Energy Efficient N+1 Transport,\u201d AIAA 2013-4327, 2013.<\/li>\n<li><strong>Takahashi, T.T.<\/strong><em>,<\/em> &#8220;Multi-Disciplinary Effects of Zero-Lift Drag and Drag Uncertainty on Aircraft Performance,&#8221; AIAA 2013-0281, 2013.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Aircraft Concept Design Performance Visualization Using an Energy-Maneuverability Presentation,&#8221; <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/Takahashi-AIAA-2012-5704-Skymaps.pdf\">AIAA-2012-5704<\/a>\u00a0, 2012.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cFederal Regulation of Electronic Flight Bags,\u201d AIAA 2012-5676, 2012. Revised version, titled \u201ciPad\u2019s in the Cockpit\u201d available at: <a href=\"http:\/\/dx.doi.org\/10.2139\/ssrn.2035743\">http:\/\/dx.doi.org\/10.2139\/ssrn.2035743<\/a><\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Law and Engineering: An Alternative Approach to Develop More Efficient Transport Category Aircraft,&#8221; AIAA 2012-0335, 2012.<\/li>\n<li>German, B.J., Patterson, M.D. and <strong>Takahashi, T.T.<\/strong>, &#8220;Reachability of Optimal Cruise Operating Points: Implications for Aircraft Design,&#8221; AIAA 2012-1036, 2012.<\/li>\n<li>German, B.J. and <strong>Takahashi, T.T.<\/strong>, &#8220;Planform as Platform: An Approach to Air Vehicle Conceptual Synthesis,&#8221; AIAA-2011-7015, 2011.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Donovan, S., \u201cNon Planar Span Loads for Minimum Induced Drag,\u201d\u00a0 \u00a0<a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/NonPlanarSpanLoadsforMinimumInducedDrag-Takahashi-AIAA-2011-0639.pdf\">AIAA-2011-0639<\/a>, 2011.<\/li>\n<li>Donovan, S. and <strong>Takahashi, T.T.<\/strong>, \u201cWing Twist Design Considerations for Transport Category Aircraft,\u201d AIAA-2011-1251, 2011<\/li>\n<li>Shajanian, A., <strong>Takahashi, T.T.<\/strong>, German, B.J., Daskilewicz, M. and Donovan, S. \u201cWing Section Thickness and Camber Allocation for Conceptual and Preliminary Aircraft Design,\u201d AIAA-2011-0164, 2011.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Donovan, S., \u201cIncorporation of Mission Payload Power and Thermal Requirements into the MDO Aircraft Performance and Sizing Process,\u201d AIAA-2010-9169, 2010.<\/li>\n<li>Donovan, S. and <strong>Takahashi, T.T.<\/strong>, \u201cA Rapid Synthesis Method to Develop Conceptual Design Transonic Wing Lofts,\u201d .\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2010-9025-RapidSynthesis.pdf\">AIAA-2010-9025<\/a>, 2010.<\/li>\n<li>Petermeier, J., Radtke, G., Stohr, M., Woodland, A., <strong style=\"font-size: 1rem;\">Takahashi, T.T.<\/strong><em style=\"font-size: 1rem;\">,<\/em><span style=\"font-size: 1rem;\"> Donovan, S. and Shubert, M., \u201cEnhanced Conceptual Wing Weight Estimation Through Structural Optimization and Simulation,\u201d <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2010-9075-Structural-Design-and-Weight-Estimation.pdf\">AIAA-2010-9075<\/a>, 2010.<\/span><\/li>\n<li>Hutchins, C., Missoum, S. and <strong>Takahashi, T.T.<\/strong>, \u201cFully Parameterized Wing Model for Preliminary Design,\u201d AIAA 2010-9120, 2010.<\/li>\n<li>Daskilewicz, M., German, B., <strong>Takahashi, T.T.<\/strong>, Donovan, S. and Shajanian, A., \u201cRobust Design Considerations in the Multi-Objective Problem of Aircraft Conceptual Design,\u201d AIAA 2010-2755, 2010.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, German, B., Shajanian, A., Daskilewicz, M., and Donovan, S., \u201cZero Lift Drag and Drag Divergence Prediction for Finite Wings in Aircraft Conceptual Design,\u201d AIAA 2010-0846, 2010.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cStrategies Teaching Configuration Aerodynamics in Aeronautical Engineering Capstone Design,\u201d AIAA 2009-1602, 2009.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cThe Search for the Optimal Wing Configuration for Small Subsonic Air Vehicles,\u201d AIAA 2008-5915, 2008.<\/li>\n<li><strong>Takahashi, T.T.,<\/strong> \u201cAeronautical Engineering Capstone Design at the University of Arizona,\u201d AIAA 2008-0494, 2008.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Fanciullo, T., and Ridgely, D.B., \u201cIncorporation of Flight Control Design Tools into the Multi-Disciplinary Conceptual Design Process,\u201d AIAA 2007-0656, 2007.<\/li>\n<li>Cunnington, R., Bays, L.V. and <strong>Takahashi, T.T.<\/strong>, \u201cIncorporation of Aerothermodynamic Analysis Tools into the Multi-Disciplinary Conceptual Design Process,\u201d\u00a0 <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA-2007-406-AerothermalTrajectory.pdf\">AIAA-2007-0406<\/a>, 2007.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, \u201cIntegrated Propulsion\/Airframe Analysis for Mission Effectiveness Driven Systems Design,\u201d AIAA 2005-4556, 2005.<\/li>\n<li>Turner, D., Birney, M. and <strong>Takahashi, T.<\/strong>, \u201cThe Effect of Mission Requirements on Propulsion Design for Advanced Weapons Systems,\u201d AIAA-2005-4196, 2005.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Spall, R.J., Turner, D.C., Birney, M.T. \u201cA Multi-Disciplinary Survey of Advanced Subsonic Tactical Cruise Missile Configurations,\u201d AIAA 2005-0709, 2005.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Spall, R.J., Turner, D.C., Otto, J.C. and O\u2019Hagan, P., \u201cA Multidisciplinary Assessment of Morphing Aircraft Structures Applied to a Cruise Missile Configuration,\u201d AIAA 2004-1725, 2004<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Coopersmith, R.M., &#8220;Wing Section Design for a Long-Range Hydrofoil Transport,&#8221; AIAA 2002-0834, 2002.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Coopersmith, R.M., &#8220;Hydrofoil Wing Section Development with High Lift Devices&#8221; AIAA 2002-0833, 2002.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Coopersmith, R.M., Novak, C.J. and Olliffe, R., &#8220;A Multidisciplinary Design Optimization of a Long-Range Hydrofoil Transport,&#8221; AIAA 2001-1106, 2001.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;Measurement of Air Flow Characteristics Using Seven Hole Cone Probes,&#8221; AIAA 97-0600, 1997.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, &#8220;On the Decomposition of Drag from Wake Survey Measurements,&#8221; AIAA 97-0717, 1997. <a href=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/AIAA97-0717-DragDecomposition.pdf\">AIAA97-0717<\/a>, 1997.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Eidson, R.C. and Heineck, J.T. &#8220;Aerodynamic Characteristics of a Supersonic Transport with Pneumatic Forebody Flow Control,&#8221; AIAA 97-0043, 1997.<\/li>\n<li>Parker, B., Eidson, R.C., <strong>Takahashi, T.T.<\/strong>, &#8220;High Speed Civil Transport Forebody Vortex Control,&#8221; AIAA 97-0042,1997.<\/li>\n<li><strong>Takahashi, T.T.<\/strong>, Parker, B., Eidson, R.C., and Heineck, J.T., &#8220;Flow Physics of a HSCT Configuration with Pneumatic Forebody Flow Control&#8221; NASA High Angle of Attack Conference, Sept. 1996.<\/li>\n<li><strong>Takahashi, T.T.<\/strong> and Ross, J.C., &#8220;On the Development of an Efficient Wake Survey System,&#8221; SAE Paper 95-1990, 1995.<\/li>\n<li>Storms, B.L., <strong>Takahashi, T.T.<\/strong> and Ross, J.C., &#8220;Aerodynamic Influence of a Finite-Span Flap on a Simple Wing,&#8221; SAE Paper 95-1977, 1995.<\/li>\n<\/ol>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-61\" src=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-375x500.jpg\" alt=\"\" width=\"375\" height=\"500\" srcset=\"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-375x500.jpg 375w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-1125x1500.jpg 1125w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-750x1000.jpg 750w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-1152x1536.jpg 1152w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-1536x2048.jpg 1536w, https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-content\/uploads\/sites\/115\/2023\/03\/2013-07-23-14.36.47-scaled.jpg 1920w\" sizes=\"auto, (max-width: 375px) 100vw, 375px\" \/><\/p>\n","protected":false},"excerpt":{"rendered":"<p class=\"mb-2\">Textbooks 1.\u00a0\u00a0\u00a0\u00a0\u00a0Takahashi, T.T., Aircraft Performance &amp; Sizing, Vol. I: Fundamentals of Aircraft Performance, Momentum Press, New York, NY, 2016. 200 pages.\u00a0ISBN-13:\u00a0978-1606506837 2.\u00a0\u00a0\u00a0\u00a0\u00a0Takahashi, T.T., Aircraft Performance &amp; Sizing, Vol. II: Applied Aerodynamic Design, Momentum Press, New York, NY, 2016. 276 pages.\u00a0ISBN-13:\u00a0978-1606509456 Traditional Journal Articles Takahashi, T.T., &#8220;On the Impact of Dispatch Weight Restrictions on Derivative Aircraft&#8230;<\/p>\n","protected":false},"author":232,"featured_media":0,"parent":0,"menu_order":2,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_acf_changed":false,"footnotes":""},"class_list":["post-18","page","type-page","status-publish","hentry"],"acf":[],"_links":{"self":[{"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/pages\/18","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/users\/232"}],"replies":[{"embeddable":true,"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/comments?post=18"}],"version-history":[{"count":3,"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/pages\/18\/revisions"}],"predecessor-version":[{"id":451,"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/pages\/18\/revisions\/451"}],"wp:attachment":[{"href":"https:\/\/labs.engineering.asu.edu\/aircraft-design\/wp-json\/wp\/v2\/media?parent=18"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}