Laminar Boundary Layer on a Spinning Cone at Small Angles of Attack in a Supersonic Flow
- 1 June 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (6) , 430-436
- https://doi.org/10.2514/8.3873
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Similarity Solution for a Spherical Shock WaveJournal of Applied Physics, 1955
- Three-Dimensional Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1953
- TESTS OF THE ELASTIC STABILITY OF A RING-STIFFENED CYLINDRICAL SHELL, MODEL BR-5 (LAMBDA= 1.705), SUBJECTED TO HYDROSTATIC PRESSUREPublished by Defense Technical Information Center (DTIC) ,1953
- Lift on Inclined Bodies of Revolution in Hypersonic FlowJournal of the Aeronautical Sciences, 1950