Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnel
- 1 September 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (9) , 1703-1705
- https://doi.org/10.2514/3.5970
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Supersonic combustion tests with a double- oblique-shock SCRAMjet ina shock tunnelAIAA Journal, 1970
- Higher-Order Boundary-Layer TheoryAnnual Review of Fluid Mechanics, 1969
- An interaction model of a supersonic laminar boundary layer on sharpand rounded backward facing steps.AIAA Journal, 1968
- Higher approximations in boundary-layer theory Part 1. General analysisJournal of Fluid Mechanics, 1962