Experimental Investigation of Supersonic Flow Past Double-Wedge Configurations
- 1 July 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (7) , 897-901
- https://doi.org/10.2514/3.60466
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Analysis of high-velocity and real-gas effects on the shock-interference pattern for delta-wing orbitersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Aerothermodynamic Aspects of Shock-Interference Patterns for Shuttle Configurations during EntryJournal of Spacecraft and Rockets, 1973
- Shock Interference Bell Aerospace, Heating in Hypersonic FlowsAIAA Journal, 1972