NASA NTRS · 20040001148
Progress in Valve Modeling at Stennis Space Center
Abstract
Understanding valve behavior will aid testing of rocket components at Stennis Space Center. The authors of this viewgraph presentation have developed a computational model for a cryogenic liquid control valve, and a gas pressure regulator valve. The model is a compressible/incompressible pressure-based FDNS code from Marshall Space Flight Center (MSFC). It is a k-epsilon turbulence model with wall functions.
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Daines, Russell L., Woods, Jody L., Sulyma, Peter. 2003-12-04. Progress in Valve Modeling at Stennis Space Center. https://ntrs.nasa.gov/citations/20040001148
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