High Temperature Rarefied Hypersonic Flow Over a Flat Plate
Author:
Affiliation:
1. General Electric Co., Schenectady , N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.5672
Reference36 articles.
1. The Free Molecule Probe and Its Use for the Study of Leading Edge Flows
2. Hypersonic Shock Wave-Boundary Layer Interaction and Leading Edge Slip
3. Hypersonic Flow Near the Leading Edge of a Flat Plate
4. The hypersonic viscous effect on a flat plate with finite leading edge
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1. Summary of Theoretical, Experimental, & Computational Investigation of Flow Over Flat Plate to Mach 25;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10
2. Viscous shock layer on a plate in hypersonic flow;European Journal of Mechanics - B/Fluids;1999-03
3. A numerical study of a viscous shock layer on a plate;Journal of Applied Mechanics and Technical Physics;1997-03
4. NPARC simulation of scramjet inlet experiments at Mach numbers from 10-20;Space Plane and Hypersonic Systems and Technology Conference;1996-11-18
5. Hypersonic flow on a flat plate. Experimental results and numerical modeling;Journal of Applied Mechanics and Technical Physics;1995-11
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