Results 131 to 140 of about 11,252 (231)

Loads and aeroelasticity division research and technology accomplishments for FY 1985 and plans for FY 1986 [PDF]

open access: yes
The Langley Research Center Loads and Aeroelasticity Division's research accomplishments for FY85 and research plans for FY86 are presented. The rk under each branch (technical area) will be described in terms of highlights of accomplishments during the ...
Dixon, S. C., Gardner, J. E.
core   +1 more source

Flutter analysis of low aspect ratio wings [PDF]

open access: yes
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic instability (flutter) characteristics. All of the wings investigated are delta planforms with clipped tips, made of aluminum alloy plate and cantilevered from
Parnell, L. A.
core   +1 more source

Wind-tunnel investigation of basic aerodynamic characteristics of a supercritical-wing research airplane configuration [PDF]

open access: yes
Transonic pressure tunnel and transonic tunnel tests were performed to determine the aerodynamic characteristics of a 0.087 scale model of a supercritical wing research airplane configuration at Mach numbers from 0.25 to 1.30.
Bartlett, D. W., Re, R. J.
core   +1 more source

Effects of dynamic aeroelasticity on handling qualities and pilot rating [PDF]

open access: yes
Pilot performance parameters, such as pilot ratings, tracking errors, and pilot comments were determined for a longitudinal pitch tracking task using a large, flexible bomber with parametric variations in the undamped natural frequencies of the two ...
Swaim, R. L., Yen, W. Y.
core   +1 more source

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