Numerical Simulation of Supersonic Boundary Layer Stability with Applied Electromagnetic Field in a Weakly Ionized Flow
Author:
Affiliation:
1. University of California
2. Innovative Scientific Solutions Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2724
Reference47 articles.
1. Palm, P., Meyer, R., Plönjes.,E., Bezant,A.,Adamovich,I.,Rich, J.W. andGogineni,S."MHD effecton a supersonicweaklyionizedflow,"AIAA-2002-2246,2002
2. Shang,J.S."AnOutlookofCEMMultidisciplinaryApplications,"AIAAPaper99-0336, 1999.
3. Canupp, P.W."The influenceofmagnetic fieldsfor shockwaves andhypersonic flows,"AIAAPaper 2000-2260,2000.
4. Damevin, H.,Dietiker,J.,andHoffmann,K. A."Hypersonic flowcomputationswithmagnetic field," AIAAPaper2000-0451,2000.
5. Agarwal, R.K., andAugustinus,J."Numericalsimulationof compressible viscous MHD flows for reducing supersonicdragofbluntbodies,"AIAAPaper99-0601,1999.
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