Free-flight simulation of the testing of supersonic inlet diffusers in a free jet wind tunnel with 50% area ratio in the Mach number range from 1.5 to 3
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Author
Contributions
- Hsu, Cheng-Ting. - Contributor
- Arnold Engineering Development Center - Contributor
Publication
1955 - Arnold Engineering Development Center, Air Research and Development Command, U.S. Air Force, Arnold Air Force Station, Tenn.
Subjects
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