Structure of swept shock wave/boundary-layer interactions using conical shadowgraphy
Author:
Affiliation:
1. Pennsylvania State University, University Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-1644
Reference16 articles.
1. Swept shock/boundary-layer interactions - Tutorial and update
2. Lu, F. K. "Fin-Generated Shock-Wave Boundary-Layer Interactions," Ph.D. Thesis,Mechanical Engineering Dept., PennsylvaniaStateuniversity,1988.
3. Kim, K.S.,Lee, Y.,Alvi, F.S., Settles, G.S., and Horstman,C.C."LaserSkin-FrictionMeasurementsand CFDComparisonofModcrate-to-Strong SweptShock/- Boundary-LayerInteractions,"AIAAPaper 90-0378,Jan. 1990.
4. Knight,D.D., Horstman, C.C.,Bogdonoff, S.M. and Shapey,B.L. "TheFlowfieldStructure of the 3-DShock Wave -BoundaryLayerInteractionGeneratedbya20° Sharp Fin at Mach 3,"A M Paper 86-0343,Jan. 1986.
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