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- 1 October 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (10), 696-704
- https://doi.org/10.2514/8.2080
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Similarity Laws for Slender Bodies of Revolution in Hypersonic FlowsJournal of the Aeronautical Sciences, 1951
- On the Nonexistence of Subsonic Conical FlowsJournal of the Aeronautical Sciences, 1951
- The Secondary Flow in a Cascade of Airfoils in a Nonuniform StreamJournal of the Aeronautical Sciences, 1951
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- Conical Flow Methods Applied to Uniformly Loaded Wings in Subsonic FlowJournal of the Aeronautical Sciences, 1951
- Turbulent Boundary-Layer Characteristics at Supersonic Speeds-Theory and ExperimentJournal of the Aeronautical Sciences, 1950
- Study of the boundary layer at supersonic speeds in turbulent flow: Case of the flow along a flat plateQuarterly of Applied Mathematics, 1950
- The air pressure on a cone moving at high speeds.—IProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1933
- On the conditions at the boundary of a fluid in turbulent motionProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1920