Navier-Stokes Simulations of a Supersonic Jet in Transonic Crossflow: Comparison to Surface Data.
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA Fluid Dynamics Conference
- Ser. no.:
- 2002
- Pub. Year:
- 2002
- No.:
- 2002-3114
- Paper no.:
- 2002-3114
- Pages:
- 16
- 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
Development of a Doppler Global Velocimeter for a Highly-Overexpanded Supersonic Jet.
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Navier- Stokes and DSMC Simulations for Hypersonic Laminar Shock- Shock Interaction Flows
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 |
10
Technical Paper
Stereoscopic PIV for Crossplane Vorticity Measurement of a Supersonic Jet in Subsonic Compressible Crossflow
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Measurement of Experimental Boundary Conditions for CFD Validation of a Supersonic Jet in Transonic Crossflow
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Turbulent Characteristics of a Transverse Supersonic Jet in a Subsonic Compressible Crossflow
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Vortex Structure Produced by a Laterally-Inclined Supersonic Jet in Transonic Crossflow
American Institute of Aeronautics and Astronautics |
12
Technical Paper
A potentially gridless solution method for the compressible Euler/Navier-Stokes equations
American Institute of Aeronautics and Astronautics |