Calculation of compressible adverse pressure gradient turbulent boundary layers.
- 1 February 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (2), 229-230
- https://doi.org/10.2514/3.6565
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- The Isobars in Boundary Layers at Supersonic SpeedsAeronautical Quarterly, 1968
- Effect of Streamwise Wall Curvature on Compressible Turbulent Boundary LayersPhysics of Fluids, 1967
- Production of longitudinal vortices in the boundary layer along a concave wallJournal of Geophysical Research, 1962