Theory of the Supersonic Turbulent Axisymmetric Near Wake behind Bluff-Base Bodies
- 1 August 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (8) , 1059-1060
- https://doi.org/10.2514/3.60754
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Theory of the Supersonic Turbulent Axisymmetric Near Wake behind Bluff-Base BodiesAIAA Journal, 1977
- Theoretical consideration of combustion effects on base pressure in supersonic flightSymposium (International) on Combustion, 1969
- An approximate pressure-angle relation for the axisymmetric supersonic near wake.AIAA Journal, 1968
- Integral theory for supersonic turbulent base flows.AIAA Journal, 1968
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- A family of similar solutions for axisymmetric incompressible wakesAIAA Journal, 1964