Gas Dynamic Gain of Supersonic Thrust Nozzles
- 1 October 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (10) , 697-704
- https://doi.org/10.2514/3.62158
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A Second-Order Bicharacteristics Method for Three-Dimensional, Steady, Supersonic FlowAIAA Journal, 1972
- Influence of Contraction Section Shape and Inlet Flow Direction on Supersonic Nozzle Flow and PerformanceJournal of Spacecraft and Rockets, 1972
- Design of rocket nozzles to reduce gas misalignment.Journal of Spacecraft and Rockets, 1968
- Exhaust Nozzle Contour for Optimum ThrustJournal of Jet Propulsion, 1958