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Experimental investigation at high subsonic speeds of the effects of leading-edge radius on the aerodynamic characteristics of a sweptback-wing - fuselage combination with leading-edge flaps and chord-extensions
Document ID
19930088723
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spreemann, Kenneth P
Date Acquired
August 29, 2013
Publication Date
July 21, 1955
Report/Patent Number
NACA-RM-L55E25a
Report Number: NACA-RM-L55E25a
Accession Number
93R18013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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