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Flight Measurements of the Pressure Distribution on the Wing of the X-1 Airplane (10 Percent Thick Wing) over a Chordwise Station near the Midspan, in Level Flight at Mach Numbers from 0.79 to 1.00 and in a Pull up at a Mach Number of 0.98
Document ID
19930086250
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Carner, H Arthur
Knapp, Ronald J
Date Acquired
August 16, 2013
Publication Date
September 12, 1950
Report/Patent Number
NACA-RM-L50H04
Accession Number
93R15540
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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