Buffet tests on 1/20 scale lca model with leading edge slats at transonic speeds [PDF]
, 1994 Buffet measurements have been made on the 1120 scale LCA model (stage 6.45 V 35) with full leading edge slat at transonic speeds in the 1.2m tunnel.
Patil, SR
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Study of lee-side flows over conically cambered delta wings at supersonic speeds, part 1 [PDF]
An experimental investigation was performed in which surface pressure data, flow visualization data, and force and moment data were obtained on four conical delta wing models which differed in leading-edge camber only.
Watson, Carolyn B., Wood, Richard M.
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An aerodynamic analysis computer program and design notes for low speed wing flap systems [PDF]
The expanded capabilities for analysis and design of low speed flap systems afforded by recent modifications of an existing computer program is described.
Carlson, H. W., Walkley, K. B.
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Design Optimization and Testing of Seamless Morphing Leading Edge for Large Civil Aircraft
Engineering ProceedingsClimate change has prompted the aviation industry to decrease its emissions of greenhouse gases. With their aerodynamic shape adaptability, morphing leading edges have great potential in the application of laminar flow wings and are beneficial to green ...
Zhigang Wang +5 more
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Subsonic balance and pressure investigation of a 60 deg delta wing with leading edge devices [PDF]
Low supersonic wave drag makes the thin highly swept delta wing the logical choice for use on aircraft designed for supersonic cruise. However, the high-lift maneuver capability of the aircraft is limited by severe induced-drag penalties attributed to ...
Rao, D. M., Tingas, S. A.
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Influence of optimized leading-edge deflection and geometric anhedral on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration [PDF]
An investigation conducted in the Langley 7 by 10 foot tunnel to determine the influence of an optimized leading-edge deflection on the low speed aerodynamic performance of a configuration with a low aspect ratio, highly swept wing.
Coe, P. L., Jr., Huffman, J. K.
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Space shuttle orbiter leading-edge flight performance compared to design goals [PDF]
, 1983 Thermo-structural performance of the Space Shuttle orbiter Columbia's leading-edge structural subsystem for the first five (5) flights is compared with the design goals.
Curry, D. M. +2 more
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Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft [PDF]
Several proposed configurations for supersonic short takeoff, vertical landing aircraft will require one or more ventral nozzles for lift and pitch control. The swivel nozzle is one possible ventral nozzle configuration.
Esker, Barbara S., Mcardle, Jack G.
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Leading Edge Technologies and Perspectives in Industrial Oilseed Extraction. [PDF]
Molecules, 2023 Cravotto C +4 more
europepmc +1 more source
A study of high-lift airfoils at high Reynolds numbers in the Langley low-turbulence pressure tunnel [PDF]
An experimental study was conducted in the Langley Low Turbulence Pressure Tunnel to determine the effects of Reynolds number and Mach number on the two-dimensional aerodynamic performance of two supercritical type airfoils, one equipped with a ...
Ferris, James C. +2 more
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