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Effects of Boattail Area Contouring and Simulated Turbojet Exhaust on the Loading and Fuselage-tail Component Drag of a Twin-engine Fighter-type Airplane ModelEffects of boattail area contouring and simulated turbojet exhaust on loading and fuselage-tail component drag of twin-engine fighter-type airplane model
Document ID
19660010757
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Foss, W. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Lee, E. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Runckel, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 14, 1958
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L58C04
Report Number: NACA-RM-L58C04
Accession Number
66N20046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC LOAD
AIRCRAFT MODEL
BOATTAIL
WING-FUSELAGE COMBINATION
FIGHTER AIRCRAFT
BODY-WING AND TAIL COMBINATION

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