Scramjet Integration on Hypersonic Research firplane Concepts
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58803
Reference9 articles.
1. Inlet performance of the integrated Langley scramjet module
2. Shock Fitting Method for Complicated Two-Dimensional Supersonic Flows
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2. Control-Relevant Modeling, Analysis, and Design for Scramjet-Powered Hypersonic Vehicles;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14
3. Flight Dynamics and Control of Air-Breathing Hypersonic Vehicles: Review and New Directions;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15
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