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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