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NASA NTRS ยท 19950017209

Adaptation of the Advanced Spray Combustion Code to Cavitating Flow Problems

Abstract

A very important consideration in turbopump design is the prediction and prevention of cavitation. Thus far conventional CFD codes have not been generally applicable to the treatment of cavitating flows. Taking advantage of its two-phase capability, the Advanced Spray Combustion Code is being modified to handle flows with transient as well as steady-state cavitation bubbles. The volume-of-fluid approach incorporated into the code is extended and augmented with a liquid phase energy equation and a simple evaporation model. The strategy adopted also successfully deals with the cavity closure issue. Simple test cases will be presented and remaining technical challenges will be discussed.

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BibTeXRIS

Liang, Pak-Yan. 1993-07-01. Adaptation of the Advanced Spray Combustion Code to Cavitating Flow Problems. https://ntrs.nasa.gov/citations/19950017209

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