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Aerodynamics / Aeronautics / Asymmetrical aircraft / Oblique wing / Mathematical optimization / Swept wing / Fixed-wing aircraft / Wing configuration / Variable-sweep wing / Aerospace engineering / Aircraft / Aviation


Comparison of Conventional and Oblique Wing Configurations for Small Supersonic Aircraft
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Document Date: 2014-06-16 01:13:10


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File Size: 1,83 MB

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City

Kriging / Palo Alto / /

Company

Lockheed1 / Desktop Aeronautics Inc. / Aerion2 / Gulfstream / the Boeing / Astronautics Inc. / Intel / Pratt and Whitney / /

Facility

Stanford University / American Institute of Aeronautics / NASA's Ames Research Center / /

IndustryTerm

nonlinear simplex search technique / aircraft preliminary design tool / correct multidisciplinary optimal solutions / obtained using the nonlinear simplex search technique / /

Organization

CG / PASS mission / American Institute of Aeronautics / Stanford University / National Aeronautics and Space Administration / /

Person

Peter Sturdza / Ilan Kroo / /

Position

fully integrated model at acceptable cost / Professor / AIAA Fellow / designer / Engineer / /

Product

CL / Gulfstream G450 / swing-wing / Oblique Wing / Concorde / swept wing / dihedral / Boeing 737 / DC-9 / /

ProgrammingLanguage

D / L / /

ProvinceOrState

California / /

SportsLeague

Stanford University / /

Technology

alpha / linear PASS algorithms / /

SocialTag