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Dynamics / Aerospace engineering / Kutta condition / Boundary layer / Drag / Lift / Inviscid flow / Airfoil / Navier–Stokes equations / Aerodynamics / Fluid dynamics / Fluid mechanics


A Rapid, Robust, and Accurate Coupled Boundary-Layer Method for Cart3D David L. Rodriguez* , Peter Sturdza† , Yoshifumi Suzuki ‡, Hervé Martins-rivas§ Desktop Aeronautics, Inc., Palo Alto, CA, 94303 Andy Peronto¶
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Document Date: 2014-06-16 01:13:10

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File Size: 3,68 MB

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City

Euler / Palo Alto / /

Company

Desktop Aeronautics Inc. / XFOIL / Douglas Aircraft Company / Design Technology / /

Event

Business Partnership / FDA Phase / /

Facility

American Institute of Aeronautics / /

IndustryTerm

analytical solution / boundary layer strip solutions / boundary-layer solution / inviscid solution / volume mesh solutions / interaction law / laminar solutions / transonic solutions / viscid and inviscid solutions / turbulent solutions / viscous solution / simultaneous solution / boundary-layer solutions / boundary layer solution / energy / quasi-simultaneous coupling algorithm / /

Organization

American Institute of Aeronautics / NASA Ames Research Center / /

Person

Hervé Martins-rivas / David L. Rodriguez / Peter Sturdza / Arthur Veldman / Yoshifumi Suzuki / /

Position

Vice President of Research & Development / Andy Peronto¶ Independent Consultant / Vice President / forward / aircraft designer / Engineer /Scientist / /

Product

NNL08AA08C / /

ProgrammingLanguage

D / /

ProvinceOrState

California / /

Technology

coupling algorithm / IBL algorithm / 3-D / quasi-simultaneous coupling algorithm / simulation / /

SocialTag