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Zero-gravity transient thermal mixing simulationThe experimental program described is an outgrowth of independent investigations into alternate redesign concepts for the Apollo SM cryogenic oxygen storage system. The experiments were continued, after the redesign was established, to provide physical insight into transient thermal mixing in zero-gravity and to aid in the characterization of the system performance in flight. Zero-gravity heat transfer and fluid mixing were simulated experimentally through an analogy between unsteady heat conduction and species diffusion. To further support numerical analyses of the cryogenic oxygen storage system, the experimental investigation was extended to include a cubical tank geometry, representative of existing numerical models. In general, the transient flow patterns in the cubical tank are far more complex than those of the spherical tank and the extent of fluid mixing is significantly greater but less repeatable.
Document ID
19720016148
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lands, J. F., Jr.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ried, R. C., Jr.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Publication Information
Publication: MSC Cryog. Symp. Papers
Subject Category
Thermodynamics And Combustion
Accession Number
72N23798
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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