Near wake of a hypersonic blunt body with mass addition
- 1 May 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (5) , 833-842
- https://doi.org/10.2514/3.5775
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Fluctuation measurements in the near wake of a wedge with and without base injection.AIAA Journal, 1969
- An experimental study of the near wake of a two-dimensional hypersonic blunt body with mass additionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Theory of laminar viscous-inviscid interactions in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Experimental and theoretical determination of flow properties in a reacting near wake.AIAA Journal, 1968
- Supersonic flow from a porous metal plate.AIAA Journal, 1968
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- A study of wakes behind a circular cylinder at m equal 5.7AIAA Journal, 1964
- Separation of Gas Mixtures in Supersonic JetsThe Journal of Chemical Physics, 1963