Reduced Order Modeling of a Rocket Engine Turbopump Inducer for Assessment of Pogo Instability
Cavitation in liquid rocket engine turbopump inducers can lead to system instabilities. One form of these flow oscillations is so-called "pogo instability", in which dynamic instability arises from the interaction of vehicle structural dynamics with thrust oscillations of a liquid fueled p...
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Massachusetts Institute of Technology
2023
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| Online Access: | https://hdl.handle.net/1721.1/153089 |