Stagnation-point heat transfer rates for pioneer-venus probes
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1998
- Pub. Year:
- 1998
- No.:
- 98-0832
- Paper no.:
- 98-0832
- Page(from):
- 1
- Page(to):
- 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 |
The American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
8
Technical Paper
Evalulation of Heat Transfer Rates of Venus Entry Capsules Along Flight Trajectories
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Simulation of Entry Flight Flowfield Over Four Probe Vehicles in Pioneer - Venus Mission.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
11
Technical Paper
Experiments on the Physical Mechanism of Heat Transfer Augmentation by Freestream Turbulence at a Cylinder Stagnation Point.
American Society of Mechanical Engineers |
6
Technical Paper
Simulation and Analysis of Stagnation Point Heat Transfer Under Free-Stream Turbulence
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |