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Full-scale wind-tunnel investigation of the low-speed static aerodynamic characteristics of a model of a reentry capsuleFull-scale wind tunnel determination of effect of corrugated canister surface on static aerodynamic characteristics of reentry capsule
Document ID
19670022826
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Scallion, W. I. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-220
Report Number: NASA-TM-X-220
Accession Number
67N32155
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STATIC AERODYNAMIC CHARACTERISTICS
WIND TUNNEL
REENTRY VEHICLE
SCALE MODEL

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