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contributor authorLee, Hyoungsoon
contributor authorPark, Ilchung
contributor authorKonishi, Christopher
contributor authorMudawar, Issam
contributor authorMay, Rochelle I.
contributor authorJuergens, Jeffrey R.
contributor authorWagner, James D.
contributor authorHall, Nancy R.
contributor authorNahra, Henry K.
contributor authorHasan, Mohammad M.
contributor authorMackey, Jeffrey R.
date accessioned2017-05-09T01:09:11Z
date available2017-05-09T01:09:11Z
date issued2014
identifier issn0022-1481
identifier otherht_136_02_021502.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/155189
description abstractFuture manned space missions are expected to greatly increase the space vehicle's size, weight, and heat dissipation requirements. An effective means to reducing both size and weight is to replace singlephase thermal management systems with twophase counterparts that capitalize upon both latent and sensible heat of the coolant rather than sensible heat alone. This shift is expected to yield orders of magnitude enhancements in flow boiling and condensation heat transfer coefficients. A major challenge to this shift is a lack of reliable tools for accurate prediction of twophase pressure drop and heat transfer coefficient in reduced gravity. Developing such tools will require a sophisticated experimental facility to enable investigators to perform both flow boiling and condensation experiments in microgravity in pursuit of reliable databases. This study will discuss the development of the Flow Boiling and Condensation Experiment (FBCE) for the International Space Station (ISS), which was initiated in 2012 in collaboration between Purdue University and NASA Glenn Research Center. This facility was recently tested in parabolic flight to acquire condensation data for FC72 in microgravity, aided by highspeed video analysis of interfacial structure of the condensation film. The condensation is achieved by rejecting heat to a counter flow of water, and experiments were performed at different mass velocities of FC72 and water and different FC72 inlet qualities. It is shown that the film flow varies from smoothlaminar to wavylaminar and ultimately turbulent with increasing FC72 mass velocity. The heat transfer coefficient is highest near the inlet of the condensation tube, where the film is thinnest, and decreases monotonically along the tube, except for high FC72 mass velocities, where the heat transfer coefficient is enhanced downstream. This enhancement is attributed to both turbulence and increased interfacial waviness. Onege correlations are shown to predict the average condensation heat transfer coefficient with varying degrees of success, and a recent correlation is identified for its superior predictive capability, evidenced by a mean absolute error of 21.7%.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Investigation of Flow Condensation in Microgravity
typeJournal Paper
journal volume136
journal issue2
journal titleJournal of Heat Transfer
identifier doi10.1115/1.4025683
journal fristpage21502
journal lastpage21502
identifier eissn1528-8943
treeJournal of Heat Transfer:;2014:;volume( 136 ):;issue: 002
contenttypeFulltext


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