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Drag Reduction Devices for Aircraft (Latest Citations from the Aerospace Database)The bibliography contains citations concerning the modeling, application, testing, and development of drag reduction devices for aircraft. Slots, flaps, fences, large-eddy breakup (LEBU) devices, vortex generators and turbines, Helmholtz resonators, and winglets are among the devices discussed. Contour shaping to ensure laminar flow, control boundary layer transition, or minimize turbulence is also covered. Applications include the wings, nacelles, fuselage, empennage, and externals of aircraft designed for high-lift, subsonic, or supersonic operation. The design, testing, and development of directional grooves, commonly called riblets, are covered in a separate bibliography.(Contains 50-250 citations and includes a subject term index and title list.)
Document ID
19980015155
Acquisition Source
Headquarters
Document Type
Other - Bibliography
Date Acquired
August 17, 2013
Publication Date
February 1, 1996
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-96-206791
PB96-863576
NAS 1.26:206790
Distribution Limits
Public
Copyright
Other
Keywords
AIRCRAFT DESIGN
BIBLIOGRAPHIES
DRAG REDUCTION
AERODYNAMIC DRAG

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