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Jang, J.H.; Faghri, A.; Chang, W.S.; Mahefkey, E.T.
National Aeronautics and Space Administration, Cleveland, OH (United States). Lewis Research Center. Funding organisation: National Aeronautics and Space Administration, Washington, DC (United States); USDOE, Washington, DC (United States); Department of Defense, Washington, DC (United States)1989
National Aeronautics and Space Administration, Cleveland, OH (United States). Lewis Research Center. Funding organisation: National Aeronautics and Space Administration, Washington, DC (United States); USDOE, Washington, DC (United States); Department of Defense, Washington, DC (United States)1989
AbstractAbstract
[en] The start-up process of a frozen heat pipe is described and a complete mathematical model for the start-up of the frozen heat pipe is developed based on the existing experimental data, which is simplified and solved numerically. The two-dimensional transient model for the wall and wick is coupled with the one-dimensional transient model for the vapor flow when vaporization and condensation occur at the interface. A parametric study is performed to examine the effect of the boundary specification at the surface of the outer wall on the successful start-up from the frozen state. For successful start-up, the boundary specification at the outer wall surface must melt the working substance in the condenser before dry-out takes place in the evaporator
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Aug 1989; 11 p; CONTRACT AI03-86SF16310; Also available from OSTI as DE94051200; NTIS; US Govt. Printing Office Dep
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