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Aerospace applications of SINDA/FLUINT at the Johnson Space CenterSINDA/FLUINT has been found to be a versatile code for modeling aerospace systems involving single or two-phase fluid flow and all modes of heat transfer. Several applications of SINDA/FLUINT are described in this paper. SINDA/FLUINT is being used extensively to model the single phase water loops and the two-phase ammonia loops of the Space Station Freedom active thermal control system (ATCS). These models range from large integrated system models with multiple submodels to very detailed subsystem models. An integrated Space Station ATCS model has been created with ten submodels representing five water loops, three ammonia loops, a Freon loop and a thermal submodel representing the air loop. The model, which has approximately 800 FLUINT lumps and 300 thermal nodes, is used to determine the interaction between the multiple fluid loops which comprise the Space Station ATCS. Several detailed models of the flow-through radiator subsystem of the Space Station ATCS have been developed. One model, which has approximately 70 FLUINT lumps and 340 thermal nodes, provides a representation of the ATCS low temperature radiator array with two fluid loops connected only by conduction through the radiator face sheet. The detailed models are used to determine parameters such as radiator fluid return temperature, fin efficiency, flow distribution and total heat rejection for the baseline design as well as proposed alternate designs. SINDA/FLUINT has also been used as a design tool for several systems using pressurized gasses. One model examined the pressurization and depressurization of the Space Station airlock under a variety of operating conditions including convection with the side walls and internal cooling. Another model predicted the performance of a new generation of manned maneuvering units. This model included high pressure gas depressurization, internal heat transfer and supersonic thruster equations. The results of both models were used to size components, such as the heaters and gas bottles and also to point to areas where hardware testing was needed.
Document ID
19930004213
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ewert, Michael K.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Bellmore, Phillip E.
(McDonnell-Douglas Space Systems Co. Houston, TX., United States)
Andish, Kambiz K.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Keller, John R.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: NASA. Lewis Research Center, The Fourth Annual Thermal and Fluids Analysis Workshop
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93N13401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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