Assessment of a Flow-Through Balance for Hypersonic Wind Tunnel Models with Scramjet Exhaust Flow Simulation
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Publication
2018 - Independently Published
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- ISBN-139781729311233
- ISBN-101729311237
- Better World Books9781729311233
- Open LibraryOL40948133M
Subjects
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