A theoretical analysis of the driver-reservoir method of driving hypersonic shock tunnels
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Author
Contributions
- Aerospace Research Laboratories (U.S.) - Contributor
Publication
1966 - Aerospace Research Laboratories, Office of Aerospace Research, United States Air Force, Wright-Patterson Air Force Base, Ohio, Ohio
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- OCLC Control Number18010356
- Open LibraryOL53856484M
Subjects
Series Statement
- ARL -- 66-0051
Other Editions
- A theoretical analysis of the driver-reservoir method of driving hypersonic shock tunnels
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