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

Show other versions (1)

© 2021 American Society of Mechanical Engineers (ASME). All rights reserved. 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, cavit...

Full description

Bibliographic Details
Main Authors: Wan, Y, Manfredi, M, Pasini, A, Spakovszky, Z
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Language:English
Published: ASME International 2021
Online Access:https://hdl.handle.net/1721.1/134548

Internet

https://hdl.handle.net/1721.1/134548

Similar Items