Measurements and computation of the triple shock wave/turbulent boundary layer interaction
Author:
Affiliation:
1. Pennsylvania State Univ., University Park
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2274
Reference28 articles.
1. Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer
2. 2)Batcho, P.F., Ketchum, A.C., Bogdonoff, S.M. and Fernando, E.M. "Preliminary Study of The Interactions Caused by CrossingShockWavesand a Turbulent BoundaryLayer,"AIAAPaper 89-0359,Jan. 1989.
3. 3)BogdonoK S.M., and Poddar, K. "An Exploratory Study of a Three-Dimensional Shock Wave Turbulent BoundaryLayerInteraction,"AIAAPaper 91-0525.
4. 5)Bogdonoff, S.M., and Stokes, W.L. "Crossing Shock Wave Turbulent Boundary Layer Interactions -Variable Angle and Shock Generator Length Geometry Effects at Mach 3,"AIAAPaper 92-0636,Jan. 1992.
5. 6)Poddar, K. and Bogdonoff, S.M. "A Study of the Unsteadinessof CrossingShockWaveTurbulentBoundary LayerInteractions,"AIAAPaper 90-1456.
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