Engineering approach to the prediction of shock patterns in bounded high-speed flows
- 1 January 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (1) , 83-90
- https://doi.org/10.2514/3.11322
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Prediction of inviscid stagnation pressure losses in supersonic inlet flowsAIAA Journal, 1990
- Steady, pseudo-steady and unsteady shock wave reflectionsProgress in Aerospace Sciences, 1988
- A reconsideration of the three-shock theory for a pseudo-steady Mach reflectionJournal of Fluid Mechanics, 1987
- Regular and Mach Reflection of Shock WavesAnnual Review of Fluid Mechanics, 1986
- Transition from regular to Mach reflection of shock waves Part 2. The steady-flow criterionJournal of Fluid Mechanics, 1982
- Further experiments on transition to Mach reflexionJournal of Fluid Mechanics, 1979
- Experiments on transition of Mach reflexionJournal of Fluid Mechanics, 1975
- Viscous slipstream flow downstream of a centerline Mach reflectionAIAA Journal, 1971
- Interaction between primary and secondary streams of supersonic ejector systems and their performance characteristicsAIAA Journal, 1964
- Triple-Shock-Wave IntersectionsPhysics of Fluids, 1959