Sinusoidally oscillating downwash and lift produced on a simple rigid airfoil were measured and compared with calculated values. Statistically stationary random downwash and the corresponding lift on a simple rigid airfoil were also measured and the transfer functions between their power spectra determined. The random experimental values are compared with theoretically approximated values. Limitations of the experimental technique and the need for more extensive experimental data are discussed
The statistical approach to the gust-load problem which consists in considering flight through turbu...
Tests have been made in the atmospheric wind tunnel of the National Advisory Committee for Aeronauti...
The damping in vaw and the directional stability of a model oscillating in yaw were measured tail-of...
Sinusoidally oscillating downwash and lift produced on a simple rigid airfoil were measured and comp...
The object of the investigation described in this report was to compare the damping coefficients of ...
Extensive experimental measurements have been made of the downwash angles and the wake characteristi...
The total lift responses to sinusoidal sinking oscillations and to sinusoidal gusts have been calcul...
Experiments have been made to determine the nature of turbulence in the wake of a two-dimensional ai...
Equations and design charts are given for predicting the downwash angles and the wake characteristic...
Measurements have been made of the lift on an airfoil in pitching oscillation with a continuous-reco...
Direct measurements were undertaken at the Aeronautics Laboratory in Turin of the aerodynamic action...
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured ...
"The new downwash measurements behind a tapered wing with parallel center section described in the p...
The present study is an analysis of the propulsive performance of a non-sinusoidally heaving airfoil...
A method is developed consistent with the assumptions of small perturbation theory which provides a ...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
Tests have been made in the atmospheric wind tunnel of the National Advisory Committee for Aeronauti...
The damping in vaw and the directional stability of a model oscillating in yaw were measured tail-of...
Sinusoidally oscillating downwash and lift produced on a simple rigid airfoil were measured and comp...
The object of the investigation described in this report was to compare the damping coefficients of ...
Extensive experimental measurements have been made of the downwash angles and the wake characteristi...
The total lift responses to sinusoidal sinking oscillations and to sinusoidal gusts have been calcul...
Experiments have been made to determine the nature of turbulence in the wake of a two-dimensional ai...
Equations and design charts are given for predicting the downwash angles and the wake characteristic...
Measurements have been made of the lift on an airfoil in pitching oscillation with a continuous-reco...
Direct measurements were undertaken at the Aeronautics Laboratory in Turin of the aerodynamic action...
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured ...
"The new downwash measurements behind a tapered wing with parallel center section described in the p...
The present study is an analysis of the propulsive performance of a non-sinusoidally heaving airfoil...
A method is developed consistent with the assumptions of small perturbation theory which provides a ...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
Tests have been made in the atmospheric wind tunnel of the National Advisory Committee for Aeronauti...
The damping in vaw and the directional stability of a model oscillating in yaw were measured tail-of...