Add to ORKGA simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms
This paper presents a new method of solution for the nite-span wings of arbitrary shapes, which avo...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation ...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation ...
Further use of the method gives downwash in the pi vertical center of the wake of the wing.A procedu...
The Weissinger method for determining additional span loading has been used to find the lift-curve s...
The Weissinger method for determining additional span loading for incompressible flow is used to fin...
A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitra...
The lifting-surface sidewash behind rolling triangular wings has been derived for a range of superso...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
The longitudinal stability characteristics of elastic swept wings of high aspect ratio experiencing ...
The method of superposition of linearized conical flows has been applied to the calculation of the a...
Charts and approximate formulas are presented for the estimation of static aeroelastic effects on th...
This paper presents a new method of solution for the nite-span wings of arbitrary shapes, which avo...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation ...
A simplified lifting-surface theory is applied to the problem of evaluating span loading due to flap...
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation ...
Further use of the method gives downwash in the pi vertical center of the wake of the wing.A procedu...
The Weissinger method for determining additional span loading has been used to find the lift-curve s...
The Weissinger method for determining additional span loading for incompressible flow is used to fin...
A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitra...
The lifting-surface sidewash behind rolling triangular wings has been derived for a range of superso...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
The longitudinal stability characteristics of elastic swept wings of high aspect ratio experiencing ...
The method of superposition of linearized conical flows has been applied to the calculation of the a...
Charts and approximate formulas are presented for the estimation of static aeroelastic effects on th...
This paper presents a new method of solution for the nite-span wings of arbitrary shapes, which avo...
A procedure based on the Weissinger method has teen devised so that the hasic span loading and assoc...
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain sta...