MHD results for argon plasma at Mach 14 and 10,600 K with a 10,300 gauss magnetic field
Author:
Affiliation:
1. Rensselaer Polytechnic Inst., Troy, NY
2. GE Research and Development Center, Schenectady, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2805
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1. Hypersonic shock-tunnel testing at an equilibrium interface condition of 4100 K
2. Myrabo, L.N.,Messitt, D.G.,and Mead, F.B. "Ground and Flight Tests of aLaser Propelled Vehicle",AIAA Paper 98-001, January 1998.
3. Magnetohydrodynamic Results for Highly Dissociated and Ionized Air Plasma
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