Experiments on Interaction of Shock Waves and Cylindrical Bodies at Supersonic Speeds
- 1 April 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (4), 237-248
- https://doi.org/10.2514/8.2238
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Visualization of Boundary-Layer FlowJournal of the Aeronautical Sciences, 1951
- III. The interaction between an oblique shock-wave and a turbulent boundary-layerJournal of Computers in Education, 1951
- REFLECTION AT A LAMINAR BOUNDARY LAYER OF A WEAK STEADY DISTURBANCE TO A SUPERSONIC STREAM, NEGLECTING VISCOSITY AND HEAT CONDUCTIONThe Quarterly Journal of Mechanics and Applied Mathematics, 1950
- Interaction Between Parallel Streams of Subsonic and Supersonic VelocitiesJournal of the Aeronautical Sciences, 1949