Add to ORKGThe approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates
Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect rati...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...
The method for determination of the spanwise lift distribution is based on the Fourier series for th...
An examination is made in this paper of a number of methods for calculating the spanwise load distri...
The approximation method described makes possible lift-distribution computations in a few minutes. C...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
As a rule, the actual lift distribution at the wing tips shows deviations from the theoretical distr...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
The finite-step method was programmed for computing the span loading and stability derivatives of tr...
A graphical method is described for finding the shape (camber and twist) of an airfoil having an arb...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...
The effect of an aileron displacement on the distribution of the lift along the span is computed for...
A method is presented for calculating lift distributions for unswept wings with flaps or ailerons us...
Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect rati...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...
The method for determination of the spanwise lift distribution is based on the Fourier series for th...
An examination is made in this paper of a number of methods for calculating the spanwise load distri...
The approximation method described makes possible lift-distribution computations in a few minutes. C...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
As a rule, the actual lift distribution at the wing tips shows deviations from the theoretical distr...
Tables are given for determining the load distribution of tapered wings with partial-span flaps plac...
The finite-step method was programmed for computing the span loading and stability derivatives of tr...
A graphical method is described for finding the shape (camber and twist) of an airfoil having an arb...
A method is presented which allows the use of nonlinear section lift data in the calculation of the ...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...
The effect of an aileron displacement on the distribution of the lift along the span is computed for...
A method is presented for calculating lift distributions for unswept wings with flaps or ailerons us...
Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect rati...
The question of the effect of distribution and magnitude of spanwise circulation and shed vorticity ...
The problem of the minimum induced drag of wings having a given lift and a given span is extended to...