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wings
1-24 of 511 Books
An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients
An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients
By Leland A. Carlson
Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis
Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis
By Leland A. Carlson
The little squeegy bug
By Bill Martin Jr.,Michael Sampson
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A. Byrdsong
Flow Modulation and Fluid-Structure Interaction at Airplane Wings
By Josef Ballmann
KC-135 Winglet Program Review
KC-135 Winglet Program Review
By KC-135 Winglet Program Review (1981 Edwards, Calif.)
Morphing aerospace vehicles and structures
Morphing aerospace vehicles and structures
By John Valasek
Flapping Wing Vehicles
By Lung-Jieh Yang,Balasubramanian Esakki
In-flight transport performance optimization
In-flight transport performance optimization
By Glenn B. Gilyard
Nonplanar wing load-line and slender wing theory
Nonplanar wing load-line and slender wing theory
By John DeYoung
Six-month progress report on an analysis of wave interactions in swept-wing flows
Six-month progress report on an analysis of wave interactions in swept-wing flows
By Helen L. Reed
Birdflight as the basis of aviation
By Otto Lilienthal
Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft
Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft
By William L White
Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50
Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50
By Jerry M. Allen
Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data
Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data
By Daryl L. Bonhaus
A transonic-small-disturbance wing design methodology
A transonic-small-disturbance wing design methodology
By Pamela S. Phillips
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
By Julio Chu