Supersonic base flow experiments in the near wake of a cylindrical afterbody
- 1 January 1994
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (1), 77-83
- https://doi.org/10.2514/3.11953
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Two-stream, supersonic, wake flowfield behind a thick base. I - General featuresAIAA Journal, 1992
- Motion of particles with inertia in a compressible free shear layerPhysics of Fluids A: Fluid Dynamics, 1991
- Turbulent flow predictions for afterbody/nozzle geometries includingbase effectsJournal of Propulsion and Power, 1991
- Supersonic flow over cylindrical afterbodies with base bleedPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Subsonic/transonic prediction capabilities for nozzle/afterbody configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Effects of External Compression on an Axisymmetric Turbulent Near WakeAIAA Journal, 1978
- Behavior of a turbulent flow, strongly out of equilibrium, at supersonic speedsPhysics of Fluids, 1977
- Mean-flow measurements in an axisymmetric compressible turbulent wake.AIAA Journal, 1968
- An Experimental Investigation of Base Flows at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1961
- A Theory for Base Pressures in Transonic and Supersonic FlowJournal of Applied Mechanics, 1956