Laminar Separation In Supersonic Flow With Emphasis On Three Dimensional Perturbations At Reattachment
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Scientific and Technical Aerospace Reports
| Author | : |
| Publisher | : |
| Total Pages | : 1460 |
| Release | : 1991 |
| Genre | : Aeronautics |
| ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Technical Publications Announcements with Indexes
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 796 |
| Release | : 1962 |
| Genre | : Aeronautics |
| ISBN | : |
Effect of Mach Number on Streamwise Vortices in Laminar Reattaching Flows
| Author | : Jean J. Ginoux |
| Publisher | : |
| Total Pages | : 40 |
| Release | : 1965 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
An experimental investigation was made in various supersonic and hypersonic wind tunnels to determine the effect of Mach number on the existence of streamwise vortices in the reattachment region of the flow over twodimensional backward facing steps. It was found that the phenomenon previously observed at M = 2.21 remained unchanged over a Mach number range of 1.5 to 7.0. The ratio of the wave length of the vortices to the boundary layer thickness at separation varied slightly with free stream Mach number, with a maximum at about M = 3. (Author).
