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
14th Annual Symposium on Propulsion ; 2002 ; State College, PA, United States
2003-12-04
Preprint
No indication
English
Progress in Valve Modeling at Stennis Space Center
NTIS | 2003
|Progress in Valve Modeling at Stennis Space Center
NTRS | 2002
|NTRS | 1992
Stennis Space Center test facilities
AIAA | 1990
|Online Contents | 1997