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Numerical Modeling of Thermofluid Transients During Chilldown of Cryogenic Transfer LinesThe chilldown of fluid transfer lines is an important part of using cryogenic systems such as those found in both ground and space based applications. The chilldown process is a complex combination of both thermal and fluid transient phenomena. A cryogenic liquid flows through a transfer line that is initially at a much higher temperature than the cryogen. Transient heat transfer processes between the liquid and transfer line cause vaporization of the liquid, and this phase change can cause transient pressure and flow surges in the liquid. As the transfer line is cooled, these effects diminish until the liquid reaches a steady flow condition in the chilled transfer line. If these transient phenomena are not properly accounted for in the design process of a cryogenic system, it can lead to damage or failure of system components during operation. For such cases, analytical modeling is desirable for ensuring that a cryogenic system transfer line design is adequate for handling the effects of a chilldown process. The purpose of this paper is to present the results of a numerical model developed using Generalized Fluid System Simulation Program (GFSSP)'s new fluid transient capability in combination with its previously developed thermal transient capability to predict pressure and flow surge in cryogenic transfer lines during a chilldown process. An experiment performed by the National Bureau of Standards (NBS) in 1966 has been chosen as the baseline comparison case for this work. NBS s experimental set-up consisted of a 10.59 cubic foot supply dewar, an inlet valve, and a 200 foot long, in Outside Diameter (OD) vacuum jacketed copper transfer line that exhausted to atmosphere. Three different inlet valves, an in-port ball valve, a 1-in-port globe valve and a 1-in-port gate valve, were used in NBS's experiments. Experiments were performed using both liquid hydrogen and liquid nitrogen as the fluids. The proposed paper will include detailed comparisons of GFSSP's predictions with NBS's experimental results.
Document ID
20030068385
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Majumdar, Alok
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Steadman, Todd
(Sverdrup Technology, Inc. Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
July 7, 2003
Subject Category
Engineering (General)
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: International Conference on Environmental Systems (ICES)
Location: Vancouver, BC
Country: Canada
Start Date: July 7, 2003
End Date: July 10, 2003
Sponsors: International Conference On Environmental Systems, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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