Add to ORKGThe statistical approach to the gust-load problem which consists in considering flight through turbulent air to be a stationary random process is extended by including the effect of lateral variation of the instantaneous gust intensity on the aerodynamic forces. The forces obtained in this manner are used in dynamic analyses of rigid and flexible airplanes free to move vertically, in pitch, and in roll. The effect of the interaction of longitudinal, vertical, and lateral gusts on the wing stresses is also considered
[[abstract]]飛機在大氣擾流中飛行,其遭受的隨機外 力衝擊造成飛機姿態角(Attitude Angle)及軌跡 (Trajectory)隨時間任意變化,運動參數時間反應 的強弱(Intens...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
A systematic procedure developed for the calculation of the structural response of aircraft flying t...
In this method, the gust velocities are represented as rolling gusts, yawing gusts, and side gusts. ...
Calculations of aerodynamic effects of an airplane encountering gusts are presented
The statistical approach to the gust-loads problem, which consists in considering flight though turb...
The report is separated into two parts. In the first part the theoretical basis for calculating the ...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
This dissertation studies the effects of turbulent wind on airplane airspeed and normal load factor,...
This dissertation studies the effects of turbulent wind on airplane airspeed and normal load factor,...
The effect of downburst-type wind shears on the longitudinal dynamic behavior of an unguided aircraf...
The data for the calculation of the air forces acting on the elevators, obtained from previous model...
[[abstract]]飛機在大氣擾流中飛行,其遭受的隨機外 力衝擊造成飛機姿態角(Attitude Angle)及軌跡 (Trajectory)隨時間任意變化,運動參數時間反應 的強弱(Intens...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
The statistical approach to the gust-load problem which consists in considering flight through turbu...
A systematic procedure developed for the calculation of the structural response of aircraft flying t...
In this method, the gust velocities are represented as rolling gusts, yawing gusts, and side gusts. ...
Calculations of aerodynamic effects of an airplane encountering gusts are presented
The statistical approach to the gust-loads problem, which consists in considering flight though turb...
The report is separated into two parts. In the first part the theoretical basis for calculating the ...
The effect of spanwise variations in gust intensity on the power spectrum directly due to atmospheri...
This dissertation studies the effects of turbulent wind on airplane airspeed and normal load factor,...
This dissertation studies the effects of turbulent wind on airplane airspeed and normal load factor,...
The effect of downburst-type wind shears on the longitudinal dynamic behavior of an unguided aircraf...
The data for the calculation of the air forces acting on the elevators, obtained from previous model...
[[abstract]]飛機在大氣擾流中飛行,其遭受的隨機外 力衝擊造成飛機姿態角(Attitude Angle)及軌跡 (Trajectory)隨時間任意變化,運動參數時間反應 的強弱(Intens...
The equations of motion for an airplane penetrating a gust are derived using a few simplifying assum...
Distributed lateral motions have been calculated for a hypothetical small airplane with various modi...