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Fluid-Structure Interaction Simulations of Rocket Engine Side Loads - 2012

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The goal of this work was to simulate both the flow in a rocket engine nozzle and the resulting flow-induced transient loads on the nozzle. This unsteady nozzle flow results in structural dynamic excitation, which contributes not only to nozzle stress and deformation but also to the dynamic loads that are transmitted to the rest of the engine.

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PDF icon Blades_ATA_final_2242012.pdf2.92 MB
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