Approximate formula of weak oblique shock wave angle
- 1 March 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (3) , 837-839
- https://doi.org/10.2514/3.10993
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
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- Three-dimensional structure of a plane mixing layerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- On the origin and evolution of streamwise vortical structures in a plane, free shear layerJournal of Fluid Mechanics, 1986
- On density effects and large structure in turbulent mixing layersJournal of Fluid Mechanics, 1974