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Modeling Unsteady Cavitation and Dynamic Loads in TurbopumpsA computational fluid dynamics (CFD) model that includes representations of effects of unsteady cavitation and associated dynamic loads has been developed to increase the accuracy of simulations of the performances of turbopumps. Although the model was originally intended to serve as a means of analyzing preliminary designs of turbopumps that supply cryogenic propellant liquids to rocket engines, the model could also be applied to turbopumping of other liquids: this can be considered to have been already demonstrated, in that the validation of the model was performed by comparing results of simulations performed by use of the model with results of sub-scale experiments in water. The need for this or a similar model arises as follows: Cavitation instabilities in a turbopump are generated as inlet pressure drops and vapor cavities grow on inducer blades, eventually becoming unsteady. The unsteady vapor cavities lead to rotation cavitation, in which the cavities detach from the blades and become part of a fluid mass that rotates relative to the inducer, thereby generating a fluctuating load. Other instabilities (e.g., surge instabilities) can couple with cavitation instabilities, thereby compounding the deleterious effects of unsteadiness on other components of the fluid-handling system of which the turbopump is a part and thereby, further, adversely affecting the mechanical integrity and safety of the system. Therefore, an ability to predict cavitation- instability-induced dynamic pressure loads on the blades, the shaft, and other pump parts would be valuable in helping to quantify safe margins of inducer operation and in contributing to understanding of design compromises. Prior CFD models do not afford this ability. Heretofore, the primary parameter used in quantifying cavitation performance of a turbopump inducer has been the critical suction specific speed at which head breakdown occurs. This parameter is a mean quantity calculated on the basis of assumed steady-state operation of the inducer; it does not account for dynamic pressure loads associated with unsteady flow caused by instabilities. Because cavitation instabilities occur well before mean breakdown in inducers, engineers have, until now, found it necessary to use conservative factors of safety when analyzing the results of numerical simulations of flows in turbopumps.
Document ID
20090011194
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
External Source(s)
http://www.techbriefs.com/component/content/article/5008
Authors
Hosangadi, Ashvin (Combustion Research and Flow Technology, Inc. Dublin, PA, United States)
Ahuja, Vineet (Combustion Research and Flow Technology, Inc. Dublin, PA, United States)
Ungewitter, Ronald (Combustion Research and Flow Technology, Inc. Dublin, PA, United States)
Dash, Sanford M. (Combustion Research and Flow Technology, Inc. Dublin, PA, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2009
Publication Information
Publication: NASA Tech Briefs, March 2009
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32586-1
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle20090011183Collected WorksNASA Tech Briefs, March 2009
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