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A WIND-TUNNEL INVESTIGATION aT SUBSONIC aND LOW SUPERSONIC SPEEDS oF a RE-ENTRY VEHICLE WITH RETRACTABLE WINGSWind tunnel tests of blunt reentry vehicle with retractable wings
Document ID
19630004028
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Smith, W. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1961
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-398
Report Number: NASA-TM-X-398
Accession Number
63N13904
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING
SUBSONIC FLOW
WIND TUNNEL STABILITY TEST
BLUNT BODY
REENTRY VEHICLE

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