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Free-flight investigation of the drag of a 60 deg delta-wing configuration with large stores mounted below the indented fuselage at mach numbers between 0.8 and 1.6Free flight drag measurements on delta wing with wing-fuselage-store
Document ID
19650003122
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Hoffman, S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1958
Subject Category
Aerodynamics
Report/Patent Number
NASA-MEMO-10-9-58L
Report Number: NASA-MEMO-10-9-58L
Accession Number
65N12723
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DRAG MEASUREMENT
DELTA WING
FREE FLIGHT
WING-FUSELAGE-STORE

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