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Experimental pressure distributions over wing tips at Mach number 1.9 II : wing tip with subsonic trailing edge
Document ID
19930086010
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mirels, Harold
Jagger, James M
Date Acquired
August 29, 2013
Publication Date
December 21, 1949
Report/Patent Number
NACA-RM-E9I22a
Report Number: NACA-RM-E9I22a
Accession Number
93R15300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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