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The study presents a frequency-domain methodology for computing the structural dynamic response of an elastic aircraft to single and ripple ejections, accounting for the time-variation of the inertial properties of the configuration.
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This page is a summary of: Dynamic Response of an Elastic Aircraft to Ripple Store Ejection, Journal of Aircraft, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035707.
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