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Mathematical Modeling of Loop Heat PipesThe primary focus of this study is to model steady-state performance of a Loop Heat Pipe (LHP). The mathematical model is based on the steady-state energy balance equations at each component of the LHP. The heat exchange between each LHP component and the surrounding is taken into account. Both convection and radiation environments are modeled. The loop operating temperature is calculated as a function of the applied power at a given loop condition. Experimental validation of the model is attempted by using two different LHP designs. The mathematical model is tested at different sink temperatures and at different elevations of the loop. Tbc comparison of the calculations and experimental results showed very good agreement (within 3%). This method proved to be a useful tool in studying steady-state LHP performance characteristics.
Document ID
19990004127
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kaya, Tarik
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Hoang, Triem T.
(TTH Research, Inc. Clifton, VA United States)
Cheung, Mark L.
(Naval Research Lab. Washington, DC United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA Paper 99-0477
Report Number: AIAA Paper 99-0477
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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