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Procedures for designing supersonic bodies of revolution from prescribed surface pressure distributionsIterative method for designing supersonic body of revolution from surface pressure distribution
Document ID
19700012050
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Barger, R. L. (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
70N21355
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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