Enhanced Range and Endurance Evaluation of a Camber Morphing Wing Aircraft. [PDF]
Jo BW, Majid T.
europepmc +1 more source
Loads and aeroelasticity division research and technology accomplishments for FY 1985 and plans for FY 1986 [PDF]
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.
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Aeroelastic flaps for dynamic airway stabilization: a novel approach to respiratory support. [PDF]
Talha M, Khalid M, Ali MKB, Waafira A.
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Flutter analysis of low aspect ratio wings [PDF]
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.
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The importance of aeroelasticity in estimating multiaxial fatigue behaviour of large floating offshore wind turbine blades. [PDF]
Sirigu M +4 more
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Data regarding the computational fluid dynamics simulations of an airfoil with plasma actuator in unsteady flow. [PDF]
De Giorgi MG, Motta V, Suma A.
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Wind-tunnel investigation of basic aerodynamic characteristics of a supercritical-wing research airplane configuration [PDF]
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.
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Wing extension-flexion coupled aeroelastic effects improve avian gliding performance. [PDF]
Wong JCM +3 more
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Modeling and analysis of long booster clustered launch-vehicle. [PDF]
Xu J, Yang Y, Fu B, Zhang D.
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Effects of dynamic aeroelasticity on handling qualities and pilot rating [PDF]
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.
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