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Computing Thermal Effects of Cavitation in Cryogenic LiquidsA computer program implements a numerical model of thermal effects of cavitation in cryogenic fluids. The model and program were developed for use in designing and predicting the performances of turbopumps for cryogenic fluids. Prior numerical models used for this purpose do not account for either the variability of properties of cryogenic fluids or the thermal effects (especially, evaporative cooling) involved in cavitation. It is important to account for both because in a cryogenic fluid, the thermal effects of cavitation are substantial, and the cavitation characteristics are altered by coupling between the variable fluid properties and the phase changes involved in cavitation. The present model accounts for both thermal effects and variability of properties by incorporating a generalized representation of the properties of cryogenic fluids into a generalized compressible-fluid formulation for a cavitating pump. The model has been extensively validated for liquid nitrogen and liquid hydrogen. Using the available data on the properties of these fluids, the model has been shown to predict accurate temperature-depression values.
Document ID
20110016393
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Hosangadi, Ashvin
(Combustion Research and Flow Technology, Inc. Huntsville, AL, United States)
Ahuja, Vineet
(Combustion Research and Flow Technology, Inc. Huntsville, AL, United States)
Dash, Sanford M.
(Combustion Research and Flow Technology, Inc. Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2005
Publication Information
Publication: NASA Tech Briefs, November 2005
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32140
Report Number: MFS-32140
Distribution Limits
Public
Copyright
Public Use Permitted.
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