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An investigation of supersonic store interference in the vicinity of a 22 deg swept wing fuselage configuration at Mach numbers of 1.61 and 2.01Pressure tunnel investigation of supersonic store interference in vicinity of 22 deg swept wing fuselage configuration at mach numbers 1.61 and 2.01
Document ID
19670022217
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Geier, D. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 24, 1958
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L57L18
Accession Number
67N31546
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPT WING
WING-FUSELAGE-STORE
AIRCRAFT CONFIGURATION
WIND TUNNEL

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