A hypersonic wake transition map.
- 1 November 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (11) , 2170-2172
- https://doi.org/10.2514/3.3341
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Technique for studying the shock-on-shock problem.AIAA Journal, 1965
- Shock-shock interaction on a slender supersonic coneJournal of Fluid Mechanics, 1965
- UNSTEADY HYPERSONIC WAKE BEHIND BLUNT BODIESAIAA Journal, 1963
- The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speedJournal of Fluid Mechanics, 1963