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THE ORIGIN AND DISTRIBUTION OF SUPERSONIC STORE INTERFERENCE FROM MEASUREMENT OF INDIVIDUAL FORCES ON SEVERAL WING-FUSELAGESTORE CONFIGURATIONS. 1.-SWEPT-WING HEAVY-BOMBER CONFIGURATION WITH LARGE STORE NACELLE . LIFT AND DRAG, MACH NUMBER, 1.61Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61
Document ID
19630003984
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Carlson, H. W. (NASA Langley Research Center Hampton, VA, United States)
Smith, N. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
March 11, 1955
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L55A13A
Accession Number
63N13860
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EXTERNAL STORE
SWEPT WING
SUPERSONIC SPEED
BOMBER AIRCRAFT

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