Dynamic model based identification of cavitation compliance and mass flow gain factor in rocket engine turbopump inducers

Dynamic model based identification of cavitation compliance and mass flow gain factor in rocket engine turbopump inducers

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Copyright © 2020 ASME. Cavitation dynamics continue to pose a significant risk in the development and operation of launch vehicle (LV) propulsion systems. In addition to generating unsteady loads that can directly damage turbopump hardware, cavitation dynamics often couple with LV fluid feed systems...

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Bibliographic Details
Main Authors: Wan, Y, Manizza, Manfredi, Pasini, A., Spakovszky, Zoltan S
Other Authors: Massachusetts Institute of Technology. Department of Mechanical Engineering
Format: Article
Language:English
Published: American Society of Mechanical Engineers 2021
Online Access:https://hdl.handle.net/1721.1/137330

Internet

https://hdl.handle.net/1721.1/137330

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