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Flow Visualization of Liquid Hydrogen Line Chilldown TestsWe present experimental measurements of wall and fluid temperature during chill-down tests of a warm cryogenic line with liquid hydrogen. Synchronized video and fluid temperature measurements are used to interpret stream temperature profiles versus time. When cold liquid hydrogen starts to flow into the warm line, a sequence of flow regimes, spanning from all-vapor at the outset to bubbly with continuum liquid at the end can be observed at a location far downstream of the cold inlet. In this paper we propose interpretations to the observed flow regimes and fluid temperature histories for two chilldown methods, viz. trickle (i.e. continuous) flow and pulse flow. Calculations of heat flux from the wall to the fluid versus wall temperature indicate the presence of the transition/nucleate boiling regimes only. The present tests, run at typical Reynolds numbers of approx O(10 (exp 5)), are in sharp contrast to similar tests conducted at lower Reynolds numbers where a well-defined film boiling region is observed.
Document ID
20140008545
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Rame, Enrique
(Universities Space Research Association Cleveland, OH, United States)
Hartwig, Jason W.
(NASA Glenn Research Center Cleveland, OH United States)
McQuillen John B.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
June 27, 2014
Publication Date
January 13, 2014
Subject Category
Physics (General)
Propellants And Fuels
Report/Patent Number
GRC-E-DAA-TN12380
Report Number: GRC-E-DAA-TN12380
Meeting Information
Meeting: AIAA SciTech 2014
Location: National Harbor, MD
Country: United States
Start Date: January 13, 2014
End Date: January 17, 2014
Sponsors: The American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 645454.04.03.01.01
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Line chill down
Two phase flow
flow visualization
Liquid hydrogen
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