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Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configurationA variable sweep bomber aircraft model was investigated to identify modifications for drag reduction. Modifications included simulated two dimensional nozzles, staggered and extended nozzles; short, long, and no interfairings between the nozzles; partial and complete wing-glove fairings; glove-fuselage sidefairing; fuselage underfairing; and wing pods. The variable wing sweep and variable exhaust nozzles of the scale model are discussed.
Document ID
19800001867
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Re, R. J. (NASA Langley Research Center Hampton, VA, United States)
Reubush, D. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-80129
L-13043
Report Number: NASA-TM-80129
Report Number: L-13043
Accession Number
80N10106
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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