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Measurement of static forces on externally carried bombs of fineness ratios 7.1 and 10.5 in the flow field of a swept-wing fighter- bomber configuration at a Mach number of 1.6Static force and interference drag on externally carried bomb in flow field of supersonic, swept wing fighter-bomber aircraft
Document ID
19660010453
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Carlson, H. W. (NASA Langley Research Center Hampton, VA, United States)
Geier, D. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 31, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L56K30
Accession Number
66N19742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
INTERFERENCE DRAG
SWEPT WING
BOMBER AIRCRAFT
FLOW FIELD
FIGHTER AIRCRAFT

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