Feasibility Study on MHD Energy Bypass Scramjet Engine
Author:
Affiliation:
1. Tokyo Institute of Technology
2. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3226
Reference13 articles.
1. Scramjet Engine Performance Attained in RJTF Testing
2. Three-Component Force Measurements for Scramjet Engines 1) Engine Drag from Mach 4 to Mach 8 Flight Conditions
3. Bityurin,V.A.andLineberry,J.T."ThermodynamicAnalysisoftheAJAXPropulsionConcept,"AIAAPaper2000-0445, 2000.
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