Add to ORKGContains charts for use in determining preliminary values of the spanwise-load, shear, bending-moment, and accumulated-torque distributions of swept wings. The charts are based on strip theory and include four aerodynamic-load distributions, two section-moment distributions, and two inertia-load distributions. The taper ratios considered cover the range from 1.0 to 0 and the results are applicable to any angle of sweep
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
Span load distributions of swept-back wings have been calculated. The method used was to replace the...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
This report presents a convenient method for calculating the pitching-moment characteristics of tape...
The Weissinger method for determining additional span loading has been used to find the lift-curve s...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
The Weissinger method for determining additional span loading for incompressible flow is used to fin...
This paper describes the derivation of empirical formulae for the loading distribution on straight t...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
Contains derivations, based on a simplified theory, of approximate relations for low-speed stability...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
This report compares the experimental force and moment data obtained by pressure measurements on a w...
Charts and approximate formulas are presented for the estimation of static aeroelastic effects on th...
An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ra...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
Span load distributions of swept-back wings have been calculated. The method used was to replace the...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-momen...
This report presents a convenient method for calculating the pitching-moment characteristics of tape...
The Weissinger method for determining additional span loading has been used to find the lift-curve s...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
The Weissinger method for determining additional span loading for incompressible flow is used to fin...
This paper describes the derivation of empirical formulae for the loading distribution on straight t...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
Contains derivations, based on a simplified theory, of approximate relations for low-speed stability...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
This report compares the experimental force and moment data obtained by pressure measurements on a w...
Charts and approximate formulas are presented for the estimation of static aeroelastic effects on th...
An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ra...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
Span load distributions of swept-back wings have been calculated. The method used was to replace the...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...