![Aerodynamics / Aeronautics / Asymmetrical aircraft / Oblique wing / Mathematical optimization / Swept wing / Fixed-wing aircraft / Wing configuration / Variable-sweep wing / Aerospace engineering / Aircraft / Aviation Aerodynamics / Aeronautics / Asymmetrical aircraft / Oblique wing / Mathematical optimization / Swept wing / Fixed-wing aircraft / Wing configuration / Variable-sweep wing / Aerospace engineering / Aircraft / Aviation](https://www.pdfsearch.io/img/e63be11c74d8c0aa2574dea03ab7ef2d.jpg)
| Document Date: 2014-06-16 01:13:10 Open Document File Size: 1,83 MBShare Result on Facebook
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 |