An analytical study was performed to define a Gust Alleviation System on a preliminary configuration of a commuter airplane. The analysis takes into account the influence of elasticity of the airplane, unsteady aerodynamic effects, mechanical nonlinearities such as backlash deadzone and control surface rate and deflection limitations. A relatively simple model shows that ride comfort can be improved by at least 50%.
Gust Alleviation on a Transport Airplane
1985
9 pages
Report
Keine Angabe
Englisch
Aerodynamics , Gust loads , Transport aircraft , Dynamic response , Aerodynamic control surfaces , Nonlinear analysis , Mathematical models , Aeroelasticity , Backlash , Deflection , Limitations , Ride quality , West germany , Italy , Gust alleviation , Unsteady aerodynamics , NATO furnished , Component reports
Gust alleviation on a transport airplane
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