Flat Plate Turbulent Boundary Layers Subject to Large Pressure Fluctuations
- 1 January 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (1) , 105-107
- https://doi.org/10.2514/3.61073
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Inviscid Flowfield Calculations for Re-entry Vehicles with Control SurfacesAIAA Journal, 1977
- Aerodynamic comparison of a conical and biconic reentry vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Hypersonic viscous static stability of a sharp 5-deg cone at incidenceAIAA Journal, 1976
- ANALYSIS OF THE ANGULAR MOTION OF MISSILES.Published by Office of Scientific and Technical Information (OSTI) ,1970