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56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Aircraft structural design is influenced by the static and dynamic loads resulting from flight manoeuvres, gust/turbulence encounters and ground manoeuvres; thus the identification of such loads is crucial for the development and structural analysis of aircraft, requiring the solution of the aeroelastic dynamic responses. Numerical aeroelastic models are used to predict a large number (1000s) of "Interesting Quantities" (IQs), and for aircraft design the identification of the worst cases fordoi:10.2514/6.2015-1847 fatcat:unzo665k7rcuxgwdkbtsc7bqii