Gust and Ground Loads Integration for Aircraft Landing Loads Prediction

Author:

Castrichini A.,Cooper J. E.,Benoit T.,Lemmens Y.

Funder

European Community, Marie Curie Initial Training Network

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference29 articles.

1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

2. Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics

3. WaszakM. R.ButtrillC. S.SchmidtD. K. “Modeling and Model Simplification of Aeroelastic Vehicles: An Overview,” NASA TM 107691, 1992.

4. MeirovitchL.TuzcuII. “Integrated Approach to the Dynamics and Control of Maneuvering Flexible Aircraft,” NASA CR-2003-211748, 2003.

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