Add to ORKGAn iteration method is presented by which the detailed aerodynamic loading and twist characteristics of a flexible wing with known elastic properties may be calculated. The method is applicable at Mach numbers approaching 1.0 as well as at subsonic Mach numbers. Calculations were made for a wing-body combination; the wing was swept back 45 deg and had an aspect ratio of 4. Comparisons were made with experimental results at Mach numbers from.0.80 to 0.98
The development in the last decades generally shows that large aircraft wings have become more light...
A method is presented for shortening the computations required to determine the steady-state span lo...
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
In this paper, means are investigated whereby the effects on loading of the shock-wave patterns and ...
Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been te...
A method similar to that of NACA rep. 1000 is presented for calculating the effectiveness and the re...
Since the aerodynamic theory is nonlinear, the method requires the coupling of two iterative process...
This report compares the experimental force and moment data obtained by pressure measurements on a w...
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...
A method is presented for calculating the aerodynamic forces on a moncylane wing, taking into accoun...
The greatest efficiency for a lifting surface at supersonic speeds, according to the theoretical con...
An analysis is presented of the effect of torsional flexibility on the rolling characteristics at su...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
Flight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplan
The development in the last decades generally shows that large aircraft wings have become more light...
A method is presented for shortening the computations required to determine the steady-state span lo...
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
In this paper, means are investigated whereby the effects on loading of the shock-wave patterns and ...
Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been te...
A method similar to that of NACA rep. 1000 is presented for calculating the effectiveness and the re...
Since the aerodynamic theory is nonlinear, the method requires the coupling of two iterative process...
This report compares the experimental force and moment data obtained by pressure measurements on a w...
A method for calculating the aerodynamic loading on a wing in combination with a body is presented. ...
A method is presented for calculating the aerodynamic forces on a moncylane wing, taking into accoun...
The greatest efficiency for a lifting surface at supersonic speeds, according to the theoretical con...
An analysis is presented of the effect of torsional flexibility on the rolling characteristics at su...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
Flight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplan
The development in the last decades generally shows that large aircraft wings have become more light...
A method is presented for shortening the computations required to determine the steady-state span lo...
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...