3 edition of Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds found in the catalog.
Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
1988 by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English
|Statement||Patsy S. Fulton.|
|Series||NASA technical memorandum -- 101531.|
|Contributions||Langley Research Center.|
|The Physical Object|
|Pagination||vi, 115 p.|
|Number of Pages||115|
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