Dynamic simulation of supersonic inlet and engine
- 10 August 1964
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Effect of Inlet Normal Shock Position Control Systems on Range of Supersonic TransportsSAE International Journal of Advances and Current Practices in Mobility, 1961