Supersonic Flow about Wedge: MHD Impact on Flow Structure and Heat Flux
Author:
Affiliation:
1. A.F.Ioffe Physical-Technical Institute RAS
2. The Johns Hopkins University, Applied Physics Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1094
Reference9 articles.
1. Relaxation of the shock-wave configuration in a diffuser after termination of the action of magnetic and electric fields
2. MHD Control of the Separation Phenomenon in a Supersonic Xenon Plasma Flow II
3. 3ThivetF.,KnightD.D.,ZheltovodovA.A.,andMaksimovA.I.InsightsinTurbulenceModelingforCross-Shock-Wave / Boundary -LayerInteractions.AIAA Journal, Vol.39,No. 6. 2001, pp. 985-995.
4. 4Fraishtadt,V.L.,Kuranov,A.L.,andSheikin,E.G.UseofMHDSysteminHypersonicAircraft.Tech.Phys.,Vol. 43, No.11, 1998, pp.1309-1313.
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