Boundarv-Layer Stability and Transition in Subsonic and Supersonic Flow
- 1 January 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (1) , 19-28
- https://doi.org/10.2514/8.2519
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Recent Investigation of Temperature Recovery and Heat Transmission on Cones and Cylinders in Axial Flow in the N.O.L. Aeroballistics Wind TunnelJournal of the Aeronautical Sciences, 1952
- Wind-Tunnel Tests for Temperature Recovery Factors at Supersonic VelocitiesJournal of the Aeronautical Sciences, 1951
- On Laminar and Turbulent Boundary Layer in Supersonic FlowReviews of Modern Physics, 1949
- A review of the statistical theory of turbulenceQuarterly of Applied Mathematics, 1943
- On transition from laminar to turbulent flow in the boundary layerProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1941
- VIII. Stability of a viscous liquid contained between two rotating cylindersPhilosophical Transactions of the Royal Society A, 1923