Shock-wave strength for separation of a laminar boundary layer at transonic speeds
- 1 June 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (6), 1197-1198
- https://doi.org/10.2514/3.6337
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Boundary-Layer Flow Near the Trailing Edge of a Flat PlateSIAM Journal on Applied Mathematics, 1970
- Self-induced separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1969
- Gravity effects on the rotational motion of a uniaxial artificial satellite.AIAA Journal, 1968
- Free Rotation of a Rigid Body Studied in the Phase PlaneAmerican Journal of Physics, 1967
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953
- On the interaction between shock waves and boundary layersMathematical Proceedings of the Cambridge Philosophical Society, 1951
- The Interaction Between Boundary Layer and Shock Waves in Transonic FlowJournal of the Aeronautical Sciences, 1946