Integrated flight loads modelling and analysis for flexible transport aircraft

Christian Reschke
This thesis is concerned with the derivation of nonlinear equations of motion for flexible aircraft in flight. These equations are intended for the accurate simulation of the flight dynamics of flexible aircraft in general and for the analysis of resulting dynamic structural loads in particular. The main focus is on the inertial coupling effects between the maneuvering flight and structural dynamics of the airframe. The field of flight loads computation is concerned with the provision...
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