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Manufacturing in space: Fluid dynamics numerical analysisNumerical computations were performed for natural convection in circular enclosures under various conditions of acceleration. It was found that subcritical acceleration vectors applied in the direction of the temperature gradient will lead to an eventual state of rest regardless of the initial state of motion. Supercritical acceleration vectors will lead to the same steady state condition of motion regardless of the initial state of motion. Convection velocities were computed for acceleration vectors at various angles of the initial temperature gradient. The results for Rayleigh numbers of 1000 or less were found to closely follow Weinbaum's first order theory. Higher Rayleigh number results were shown to depart significantly from the first order theory. Supercritical behavior was confirmed for Rayleigh numbers greater than the known supercritical value of 9216. Response times were determined to provide an indication of the time required to change states of motion for the various cases considered.
Document ID
19830004859
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Robertson, S. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Nicholson, L. A.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Spradley, L. W.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Astronautics (General)
Report/Patent Number
NAS 1.26:169536
NASA-CR-169536
LMSC-HREC-TR-D867640
Report Number: NAS 1.26:169536
Report Number: NASA-CR-169536
Report Number: LMSC-HREC-TR-D867640
Accession Number
83N13129
Funding Number(s)
CONTRACT_GRANT: NASW-3281
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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