Shock-Tube Studies of Transonic Flow over Wedge Profiles
- 1 April 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (4) , 249-257
- https://doi.org/10.2514/8.2242
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Transonic Flow Past Wedge SectionsJournal of the Aeronautical Sciences, 1950
- The Flow over a Wedge Profile at Mach Number 1Journal of the Aeronautical Sciences, 1950
- Photo-Conductivity in Amorphous SeleniumPhysical Review B, 1950
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- Interaction of Shock WavesReviews of Modern Physics, 1949
- Airfoils in Slightly Supersonic FlowJournal of the Aeronautical Sciences, 1949
- An Investigation of the Detached Shock in Front of a Body of RevolutionJournal of the Aeronautical Sciences, 1948
- On the Flow Behind Curved ShocksJournal of Mathematics and Physics, 1948
- The Similarity Law of Transonic FlowJournal of Mathematics and Physics, 1947