A Theoretical Investigation of Laminar Separation in Supersonic Flow
- 1 October 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (10), 759-771
- https://doi.org/10.2514/8.3959
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- An experimental investigation of heat transfer effects on boundary layer separation in supersonic flowJournal of Fluid Mechanics, 1957
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953
- Temperature Gradients in Turbulent Gas StreamsIndustrial & Engineering Chemistry, 1953