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A New Unsteady Model for Dense Cloud Cavitation in Cryogenic FluidsA new unsteady, cavitation model is presented wherein the phase change process (bubble growth/collapse) is coupled to the acoustic field in a cryogenic fluid. It predicts the number density and radius of bubbles in vapor clouds by tracking both the aggregate surface area and volume fraction of the cloud. Hence, formulations for the dynamics of individual bubbles (e.g. Rayleigh-Plesset equation) may be integrated within the macroscopic context of a dense vapor cloud i.e. a cloud that occupies a significant fraction of available volume and contains numerous bubbles. This formulation has been implemented within the CRUNCH CFD, which has a compressible real fluid formulation, a multi-element, unstructured grid framework, and has been validated extensively for liquid rocket turbopump inducers. Detailed unsteady simulations of a cavitating ogive in liquid nitrogen are presented where time-averaged mean cavity pressure and temperature depressions due to cavitation are compared with experimental data. The model also provides the spatial and temporal history of the bubble size distribution in the vapor clouds that are shed, an important physical parameter that is difficult to measure experimentally and is a significant advancement in the modeling of dense cloud cavitation.
Document ID
20050209921
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hosangadi, A.
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Ahuja, V.
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Date Acquired
September 7, 2013
Publication Date
June 9, 2005
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2005-5347
Report Number: AIAA Paper 2005-5347
Meeting Information
Meeting: 17th AIAA Computational Fluid Dynamics Conference
Location: Toronto, Ontario
Country: Canada
Start Date: June 6, 2005
End Date: June 9, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM05AA05C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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