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Drag Interference Between a Pointed Cylindrical Body and Triangular Wings of Various Aspect Ratios at Mach Numbers of 1.50 and 2.02The drag of a body alone, six triangular wings of various aspect ratios, and the combinations were measured at Mach numbers of 1.50 and 2.02 at a Reynolds number of 5.5 million (based on the body length). The experimental drag-interference results were in accordance with calculations based on NACA RM A9E19, 1949, with skin-friction effects taken into account, the interference effect being principally the result of fixing transition on the body by adding a wing.
Document ID
19930084518
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Katzen, Elliott D
Kaattari, George E
Date Acquired
August 16, 2013
Publication Date
November 1, 1956
Report/Patent Number
NACA-TN-3794
Accession Number
93R13808
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BODIES
WINGS, COMPLETE - ASPECT RATIO
WING-BODY COMBINATIONS - MISSILES
WING-FUSELAGE COMBINATIONS - AIRPLANES

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