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Heat Entrapment Effects Within Liquid Acquisition DevicesWe introduce a model problem to address heat entrapment effects or the local accumulation of thermal energy within liquid acquisition devices. We show that the parametric space consists of six parameters, namely the Rayleigh and Prandtl numbers, the aspect ratio, and heat flux ratios for the bottom, side, and top boundaries of the enclosure. For the range of Ra considered 1 to 10(sup 9), beyond Ra on the order of 10(sup 5), convective instability is the dominant mode of convection in comparison to natural convection. The flow field transitions to asymmetric modes at Ra on the order of 10(sup 7). Direct numerical simulation of a large geometric length scale prototype for Ra on the order of 10(sup 9) shows that the flow field evolves from small wavelength instability which gives rise to nonlinear growth of thermals, propagation of the instability occurs via growth of secondary and tertiary modes, and a travelling wave mode occurs prior to asymmetry. The effect of a large aspect ratio is to increase the number of modes in the vertical direction. Due to the slow diffusion of heat in the prototype, asymptotic states are not readily attained, we show that dynamical similarity can be used for a model which allows the attainment of asymptotic states and that transition to a chaotic state occurs for Ra on the order of 10(sup 9) via a broadband power spectrum. These dynamical events show that for the baseline condition in which heat is absorbed from background laboratory environment, higher heat flux is absorbed at the top and bottom boundaries of the enclosure than a nominal value of 34.9 ergs per square centimeter -second.
Document ID
20100039309
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Duval, W. M. B.
(NASA Glenn Research Center Cleveland, OH, United States)
Chato, D. J.
(NASA Glenn Research Center Cleveland, OH, United States)
Doherty, M. P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
September 1, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-17188
E-17188-1
NASA/TM-2010-216789
NASA/TM-2010-216789REV1
AIAA Paper 2010-1298
Report Number: E-17188
Report Number: E-17188-1
Report Number: NASA/TM-2010-216789
Report Number: NASA/TM-2010-216789REV1
Report Number: AIAA Paper 2010-1298
Meeting Information
Meeting: 48Th AIM Aerospace Scieces Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2010
End Date: January 7, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 095240.04.03.03.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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