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    Experimental Investigation of Flow Condensation in Microgravity

    Source: Journal of Heat Transfer:;2014:;volume( 136 ):;issue: 002::page 21502
    Author:
    Lee, Hyoungsoon
    ,
    Park, Ilchung
    ,
    Konishi, Christopher
    ,
    Mudawar, Issam
    ,
    May, Rochelle I.
    ,
    Juergens, Jeffrey R.
    ,
    Wagner, James D.
    ,
    Hall, Nancy R.
    ,
    Nahra, Henry K.
    ,
    Hasan, Mohammad M.
    ,
    Mackey, Jeffrey R.
    DOI: 10.1115/1.4025683
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Future 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%.
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      Experimental Investigation of Flow Condensation in Microgravity

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    http://yetl.yabesh.ir/yetl1/handle/yetl/155189
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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