Time Spectral Method for Rotorcraft Flow with Vorticity Confinement
- Author(s):
- N. Butsuntorn ( Stanford University, Stanford, CA )
- A. Jameson
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- 2008
- Pub. Year:
- 2008
- No.:
- 2008-7340
- Paper no.:
- AIAA 2008-7340
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200810 [CD-ROM 2008 Disc 10]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
EFFICIENT EULERIAN COMPUTATION OF REALISTIC ROTORCRAFT FLOWS USING VORTICITY CONFINEMENT A Survey of Recent Results
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Time Spectral Method for Periodic Unsteady Computations over Two- and Three- Dimensional Bodies
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Large Eddy Simulation of Compressible Turbulent Channel Flow with Spectral Difference method
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Towards a Better Understanding of Vorticity Confinement Methods in Compressible Flow
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
The Computation of Massively Separated Flows Using Compressible Vorticity Confinement Methods.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
A p-Multigrid Spectral Difference Method for Viscous Compressible Flow using 2D Quadrilateral Meshes
American Institute of Aeronautics and Astronautics |