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Analysis of the flow field of a jet in a subsonic crosswindJet induced flow field effects on V/STOL aircraft in subsonic transition flight
Document ID
19700012075
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Margason, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publication: L. METHODS IN AIRCRAFT AERODYN. 1970
Subject Category
Aerodynamics
Accession Number
70N21380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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