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Fluid mechanics / Vortex lattice method / Vortex / Lift / Drag / Wing / Wind tunnel / Fixed-wing aircraft / Kutta condition / Aerodynamics / Aerospace engineering / Fluid dynamics


Comparing Aerodynamic Models for Numerical Simulation of Dynamics and Control of Aircraft Christopher J. Sequeira∗ and David J. Willis∗ Jaime Peraire† Massachusetts Institute Of Technology, 77 Massachusetts Ave., C
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Document Date: 2006-02-01 15:02:27

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City

Cambridge / /

Country

United States / /

Facility

American Institute of Aeronautics / David J. Willis∗ Jaime Peraire† Massachusetts Institute Of Technology / tunnel Positive / /

IndustryTerm

potential flow solution / freedom rigid body dynamics simulation tool / unsteady potential flow solutions / dynamics tool / behavioral estimation tool / /

Organization

Massachusetts Institute of Technology / Department of Aeronautics and Astronautics / American Institute of Aeronautics / /

Person

David J. Willis / Euler / /

Position

Forward / Professor / /

Product

CL / lifting body / canard / /

ProgrammingLanguage

C++ / /

ProvinceOrState

Massachusetts / /

Technology

radiation / Simulation / API / /

SocialTag