Aeroelastic phenomena arising from the interaction of aerodynamic, elastic, and inertial forces, and the loads resulting from flight/ground maneuvers and gust/turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response, and loads requires application of a range of interrelated engineering disciplines.
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Aeroelastic phenomena arising from the interaction of aerodynamic, elastic, and inertial forces, and the loads resulting from flight/ground maneuvers and gust/turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response, and loads requires application of a range of interrelated engineering disciplines.
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