Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
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Author
Contributions
- Langley Research Center. - Contributor
Publication
1994 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18079126M
Alternate Titles
- Wind tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6.
Subjects
Series Statement
- NASA technical memorandum -- 109152.
Other Editions
- Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
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