A note on experimental and theoretical comparisons of conical shock-shock interactions.
- 1 November 1966
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (11), 2054-2056
- https://doi.org/10.2514/3.3846
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Experiments on the head-on shock-shock interaction.AIAA Journal, 1965
- Technique for studying the shock-on-shock problem.AIAA Journal, 1965
- Interaction of a shock wave and a wedge - an application of the hydraulic analogyAIAA Journal, 1965
- Shock-shock interaction on a slender supersonic coneJournal of Fluid Mechanics, 1965
- Viscous Hypersonic Flow Past a Slender ConePhysics of Fluids, 1964
- CRITERION FOR SLIP NEAR THE LEADING EDGE OF A FLAT PLATE IN HYPERSONIC FLOWAIAA Journal, 1963
- The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speedJournal of Fluid Mechanics, 1963
- EFFECT OF SLIGHT LEADING EDGE BLUNTING ON HYPERSONIC FLOWS PAST BODIESPublished by Elsevier ,1961
- Molecular Flow of GasesPhysics Today, 1956
- The diffraction of blast. IProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949