Accurate prediction of gust stress being out of the question because of the multiplicity of the free air movements, the exploration of gust stress is restricted to static method which must be based upon: 1) stress measurements in free flight; 2) check of design specifications of approved type airplanes. With these empirical data the stress must be compared which can be computed for a gust of known intensity and structure. This "maximum gust" then must be so defined as to cover the whole ambit of empiricism and thus serve as prediction for new airplane designs
The observed gust experience of an airplane and information on the associated meteorological conditi...
Available measurements of the derived gust velocities within thunderstorms are summarized for altitu...
An analytical study of the effects of wing flexibility on wing strains due to gusts has been made fo...
Accurate prediction of gust stress being out of the question because of the multiplicity of the free...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
A revised gust-load formula with a new gust factor is derived to replace the gust-load formula and a...
Past history, present status, and future of discrete gusts are schematically presented. It is shown ...
Calculations of aerodynamic effects of an airplane encountering gusts are presented
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A brief review is presented of the basic methods of gust alleviation. Some results obtained in fligh...
This project presents work performed by the Institute of Aerospace Engineering, Brno University of T...
In this report it is shown that determining the instantaneous angle of pitch, the acceleration of th...
On the wing structures of modern high speed aircraft, in particular, the comparatively high-service ...
Measurements of gust structure and gust intensity were made in the lower levels of the atmosphere (0...
The observed gust experience of an airplane and information on the associated meteorological conditi...
Available measurements of the derived gust velocities within thunderstorms are summarized for altitu...
An analytical study of the effects of wing flexibility on wing strains due to gusts has been made fo...
Accurate prediction of gust stress being out of the question because of the multiplicity of the free...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
A revised gust-load formula with a new gust factor is derived to replace the gust-load formula and a...
Past history, present status, and future of discrete gusts are schematically presented. It is shown ...
Calculations of aerodynamic effects of an airplane encountering gusts are presented
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A brief review is presented of the basic methods of gust alleviation. Some results obtained in fligh...
This project presents work performed by the Institute of Aerospace Engineering, Brno University of T...
In this report it is shown that determining the instantaneous angle of pitch, the acceleration of th...
On the wing structures of modern high speed aircraft, in particular, the comparatively high-service ...
Measurements of gust structure and gust intensity were made in the lower levels of the atmosphere (0...
The observed gust experience of an airplane and information on the associated meteorological conditi...
Available measurements of the derived gust velocities within thunderstorms are summarized for altitu...
An analytical study of the effects of wing flexibility on wing strains due to gusts has been made fo...