On the Existence of a Pressure Plateau in Pure Laminar Separated Flows
- 1 August 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (8) , 1503-1504
- https://doi.org/10.2514/3.55281
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Thermally induced vibrations of thin nonshallow spherical shells.AIAA Journal, 1966
- LAMINAR BOUNDARY-LAYER SEPARATION ON FLARED BODIES AT SUPERSONIC AND HYPERSONIC SPEEDSPublished by Defense Technical Information Center (DTIC) ,1965
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Dynamic Response of Beams and Plates to Rapid HeatingJournal of Applied Mechanics, 1957
- The Determination of Temperature, Stresses, and Deflections in Two-Dimensional Thermoelastic ProblemsJournal of the Aeronautical Sciences, 1956
- An experimental investigation of the interaction between shock waves and boundary layersProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1954