Three-Dimensional Simulation of Transverse Injection in a Supersonic Flow by the CESE Method.
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2003
- Pub. Year:
- 2003
- No.:
- 2003-0375
- Paper no.:
- 2003-0375
- Pages:
- 10
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Three-Dimensional Dynamic Characteristics of Transverse Fuel Injection Into Supersonic Crossflow
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Direct Calculations of One-, Two-, and Three-Dimensional Detonations by the CESE Method
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Direct Calculation of High-Speed Cavity Flows in a Scramjet Engine by the CESE Method.
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Three-Dimensional Simulations of Detonations by the CE/SE Method Using a Low-Cost Beowulf Cluster
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Simulation of Shock-Tube Flows with Detailed Finite-Rate Chemistry by the CESE Method
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Application of the CESE Method to Detonation with Realistic Finite-Rate Chemistry.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |