Transonic flow field around the CF-18 wing at angle of attack 4.5°
- Author(s):
- Tang, F.C. ( Institute for Aerospace Research National Research Council )
- Jiang, L.Y.
- Ohman, L.H.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-0797
- Paper no.:
- 00-0797
- Page(from):
- 1
- Page(to):
- 9
- 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
Assessment of turbulence models for the transonic flow around the DLR-F4 wing/body configuration
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
In-Flight Flow visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack
National Aeronautics and Space Adminstration |
4
Technical Paper
Computation of Flow and Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:1, AR=1:2, AR=1:4) with 45-Deg Angled Ribs by a Reynolds Stress Turbulence …
American Society of Mechanical Engineers |
10
Technical Paper
Semiempirical Analysis of Limit Cycle Oscillation from Transonic Flow-State Changes at Angle of Attack
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Prediction of Wind Tunnel Effects on the Installed F/A-18A Inlet Flow Field at High Angles-of-Attack
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Study of the Flow Around An External Fuel Tank Mounted Under a CF-18 Wing Using Combined PSP and Schlieren Techniques
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |