The total lift responses to sinusoidal sinking oscillations and to sinusoidal gusts have been calculated, largely from existing information, for wings of various plan forms in subsonic and supersonic flow. For most of the cases considered, closed-form expressions are given and the final results are presented in the form of plots of the square of the modulus of the lift coefficient for wings in a sinusoidally oscillating gust field and in the form of the real and imaginary parts of the lift coefficient for wings undergoing sinusoidal sinking oscillations
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
Cover title."February 1963."Includes bibliographical references.Mode of access: Internet
The variation of pressure distribution is calculated for a two-dimensional supersonic airfoil either...
The total lift responses to sinusoidal sinking oscillations and to sinusoidal gusts have been calcul...
Numerical lifting-surface method to calculate direct gust forces and moments on wings at subsonic sp...
Unsteady-lift functions for wings of finite aspect ratio have been calculated by correcting the aero...
The variation of pressure distribution is calculated for a two-dimensional supersonic airfoil either...
The object of this report is to provide an estimate, based on theoretical calculations, of the force...
Sinusoidally oscillating downwash and lift produced on a simple rigid airfoil were measured and comp...
Details are given of a numerical solution of the integral equation which relates oscillatory or stea...
a summary is given of the principal results on air forces for a wing undergoing unsteady motion in a...
Linearized theory for compressible unsteady flow is used to derive the velocity potential and lift a...
A numerical study of the response of aircraft wings to atmospheric gusts and to nuclear explosions w...
A first order in frequency theory is developed for the aerodynamic loads on a harmonically oscillati...
A first order in frequency theory is developed for the aerodynamic loads on a harmonically oscillati...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
Cover title."February 1963."Includes bibliographical references.Mode of access: Internet
The variation of pressure distribution is calculated for a two-dimensional supersonic airfoil either...
The total lift responses to sinusoidal sinking oscillations and to sinusoidal gusts have been calcul...
Numerical lifting-surface method to calculate direct gust forces and moments on wings at subsonic sp...
Unsteady-lift functions for wings of finite aspect ratio have been calculated by correcting the aero...
The variation of pressure distribution is calculated for a two-dimensional supersonic airfoil either...
The object of this report is to provide an estimate, based on theoretical calculations, of the force...
Sinusoidally oscillating downwash and lift produced on a simple rigid airfoil were measured and comp...
Details are given of a numerical solution of the integral equation which relates oscillatory or stea...
a summary is given of the principal results on air forces for a wing undergoing unsteady motion in a...
Linearized theory for compressible unsteady flow is used to derive the velocity potential and lift a...
A numerical study of the response of aircraft wings to atmospheric gusts and to nuclear explosions w...
A first order in frequency theory is developed for the aerodynamic loads on a harmonically oscillati...
A first order in frequency theory is developed for the aerodynamic loads on a harmonically oscillati...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
Cover title."February 1963."Includes bibliographical references.Mode of access: Internet
The variation of pressure distribution is calculated for a two-dimensional supersonic airfoil either...