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Aerodynamic characteristics in pitch of a modified half ring wing body combination and a swept wing body combination at Mach 2.16 to 3.70Wind tunnel stability tests of pinch of modified half ring wing body and swept wing body combinations at supersonic speeds
Document ID
19680012471
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lamb, M. (NASA Lewis Research Center Cleveland, OH, United States)
Morris, O. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1551
Report Number: NASA-TM-X-1551
Accession Number
68N21940
Funding Number(s)
CONTRACT_GRANT: 126-13-02-08-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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