Characteristic Variable Boundary Conditions for Arbitrary Mach Number Algorithm in Rotating Frame
- Author(s):
- Publication title:
- A collection of technical papers : 16th AIAA Computational Fluid Dynamics Conference, Orlando, Florida 23-26 June 2003
- Title of ser.:
- AIAA Paper : AIAA Computational Fluid Dynamics Conference
- Ser. no.:
- 2003
- Pub. Year:
- 2003
- Vol.:
- v. 2
- No.:
- 2003-3976
- Paper no.:
- AIAA-2003-3976
- Page(from):
- 1302
- Page(to):
- 1313
- Pages:
- 12
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563475993 [1563475995]
- Language:
- English
- Call no.:
- A07400/033424 (v.2)
- Type:
- Technical Paper
Similar Items:
American Society of Mechanical Engineers |
7
Technical Paper
Aerodynamic Analysis of a Spinning Missile with Dithering Canards Using a High Order Unstructured Grid Scheme
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Numerical Simulation and Experiment Comparison of Leading-Edge Receptivity of A Mach 5.92 Boundary Layer
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
9
Technical Paper
Low-speed Characteristics of a High Subsonic Mach Number OHS Aircraft Configuration.
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Robust and simple non-reflecting boundary conditions for the space-time conservation element and solution element method
American Institute of Aeronautics and Astronautics |
10
Technical Paper
A High Order Cut-Cell Method for Numerical Simulation of Hypersonic-Boundary Transition with Arbitrary Surface Roughness
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |