Design, Tests, and Verification of a Diffuser System for a Mach 4 Scramjet Test Facility
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/10.2514/3.58583
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Unstart phenomena induced by flow choking in scramjet inlet-isolators;Progress in Aerospace Sciences;2018-02
2. Scramjet development and testing in the United States;10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference;2001-04-24
3. Starting and test rhombus characteristics of two-dimensional supersonic free-jet nozzle/generic supersonic aircraft inlet configurations;AlAA 4th International Aerospace Planes Conference;1992-08-17
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