Comparative Analysis of MHD and Plasma Methods of Scramjet Inlet Control
Author:
Affiliation:
1. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-170
Reference37 articles.
1. Kuranov, A.L., and Sheikin, E.G. "MHD Control on Hypersonic Aircraft under AJAX Concept: PossibilitiesofMHDGenerator,"AIAAPaper2002-0490,2002.
2. Macheret, S. O., Shneider, M. N., and Miles, R. B. "Scramjet Inlet Control by Off-Body Energy Addition: a Virtual Cowl," AIAA Paper 2003-0032,41stAIAA Aerospace Sciences Meeting and Exhibit, 6-9January2003,Reno,Nevada.
3. Vatazhin, A., Kopchenov, V., and Gouskov, O. "Some Estimations of Possibility to Use the MHD ControlforHypersonicFlowDeceleration,"AIAAPaper99-4972,1999.
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