RESEARCH STUDY TO VERIFY AND EXTEND HIGH SPEED MATH MODEL FOR JET REACTION CONTROL EFFECTIVENESS.
MARTIN CO ORLANDO FLA
Pagination or Media Count:
An analytical model was developed to predict the performance of a two-dimensional, reaction control jet exhausting normal to supersonic and hypersonic streams. The separation of a turbulent boundary layer upstream of the jet and the pressure field downstream of the jet were studied. A wind tunnel test of a jet slot on a flat plate model was conducted. The existing flow model was revised to give improved accuracy of the predictions of the interference effects upstream of the jet. The flow model was extended to include interference effects downstream of the jet. Author
- Fluid Mechanics