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Measurements of Fluctuating Pressures on a 1/4-scale Model of the X-1 Airplane with a 10-percent-thick Wing in the Langley 16-foot Transonic Tunnel
Document ID
19930087362
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Habel, Louis W
Steinberg, Seymour
Date Acquired
August 16, 2013
Publication Date
January 7, 1953
Report/Patent Number
NACA-RM-L52J31
Report Number: NACA-RM-L52J31
Accession Number
93R16652
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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