Flow Immediately behind a Step in a Simulated Supersonic Combustor
- 1 September 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (9) , 1143-1148
- https://doi.org/10.2514/3.60521
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Wall Shear and Boundary-Layer Measurements in Shock Seperated FlowAIAA Journal, 1974
- Structure of Shock Waves in Cylindrical DuctsAIAA Journal, 1973
- Prediction of Precombustion Wall Pressure Distributions in Scramjet EnginesJournal of Spacecraft and Rockets, 1973
- Liquid Jet Injection into a Supersonic FlowAIAA Journal, 1973
- An experimental study of supersonic flow over a rearward facing step.AIAA Journal, 1967