External heat supply in a detonation wave
Abstract
The problem of hypersonic flow about the double wedge airfoil with an external heat supply in a detonation wave was investigated. It is found that the correct amount of boundary conditions for the flow leads to an essential decrease in the thrust. Other topics discussed include supersonic flow, lift, mathematical models, and heat transfer.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- January 1975
- Bibcode:
- 1975STIN...7522653B
- Keywords:
-
- Detonation Waves;
- Heat Transfer;
- Hypersonic Flow;
- Airfoil Profiles;
- Jet Lift;
- Mathematical Models;
- Thrust Measurement;
- Wedges;
- Fluid Mechanics and Heat Transfer