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.
Progress in Valve Modeling at Stennis Space Center
2003
17 pages
Report
Keine Angabe
Englisch
Progress in Valve Modeling at Stennis Space Center
NTRS | 2003
|Progress in Valve Modeling at Stennis Space Center
NTRS | 2002
|NTRS | 1992
Stennis Space Center test facilities
AIAA | 1990
|Stennis Space Center test facilities
NTRS | 1990
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