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THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WINGFUSELAGE-STORE CONFIGURATIONS. IV.-DELTA-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE. MACH NUMBER, 1.61Origin and distribution of supersonic store interference/measurement of individual forces on delta-wing heavy bomber configuration mach 1.61
Document ID
19630003995
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Morris, O. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
December 15, 1955
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L55I27a
Report Number: NACA-RM-L55I27a
Accession Number
63N13871
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
EXTERNAL STORE
AERODYNAMIC FORCE
BOMBER AIRCRAFT
WING-FUSELAGE-STORE
DELTA WING

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