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Navier-Stokes flow field analysis of compressible flow in a high pressure safety relief valveThe objective of this study is to investigate the complex three-dimensional flowfield of an oxygen safety pressure relieve valve during an incident, with a computational fluid dynamic (CFD) analysis. Specifically, the analysis will provide a flow pattern that would lead to the expansion of the eventual erosion pattern of the hardware, so as to combine it with other findings to piece together a most likely scenario for the investigation. The CFD model is a pressure based solver. An adaptive upwind difference scheme is employed for the spatial discretization, and a predictor, multiple corrector method is used for the velocity-pressure coupling. The computational result indicated vortices formation near the opening of the valve which matched the erosion pattern of the damaged hardware.
Document ID
19950024441
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vu, Bruce
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wang, Ten-See
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Shih, Ming-Hsin
(Mississippi State Univ. Mississippi State, MS., United States)
Soni, Bharat
(Mississippi State Univ. Mississippi State, MS., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:110640
NASA-TM-110640
Report Number: NAS 1.15:110640
Report Number: NASA-TM-110640
Accession Number
95N30862
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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