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Transient flow features and effects of fluid-structure interaction can cause severe loads and damages in rocket engine nozzles. Different mechanisms contributing to the overall aeroelastic stability of a scaled nozzle experiment were isolated and investigated in detail by comparison to simplified setups.
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This page is a summary of: Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle, Journal of Propulsion and Power, September 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b39178.
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