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Abstract
In this paper, unit heat pipe receiver in advanced solar dynamic system was numerically simulated. Accordingly, mathematical model was set up, numerical calculation method was offered, numerical results were compared with the experimental results concerned. The temperature field of PCM (Phase Change material) was shown, the thermal performance of heat pipe receiver was analyzed. Analysis results show the axial and radial temperature difference of heat pipe are small; the thermal performance of heat pipe receiver is stable and reliable. The existence of void cavity influences the process of phase change; the temperature gradient of PCM zone is very significant because of the effect of void cavity.
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References
- Dennis Alexander., "2KV Solar Dynamic Ground Test Demonstration Project", Report. NASA-CR198423, Tempe. Arizona, Allied Signal Aerospace, 1997.
- "Solar Dynamic Power System Development for Space Station Freedom", Report. NASA-RP-1310, N94-12807, Cleveland, Ohio, Lewis Research Center, 1993.
- Hal J. Strumpf., "On-Orbit Performance Prediction of the Heat Receiver for the U.S/Russia Solar Dynamic Power Flight Experiment", Journal. IEEE, 1996.
- Marvin Warshay and Thaddeus Smog., "The NASA Advanced Solar Dynamic Technology Program", IEEE, 1989.
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- Anthony, P., "Advanced Solar Brayton Space Power Systems", Report. IECEC Paper 899492.
- Hal J. Strumpf and Chiristopher Krystkowiak., "Design of the Heat Receiver for the US/Russia Solar
- Dynamic Power Joint Flight Demonstration", Report. IECEC Paper, 1995, pp.411-416.
- Strumpf, H.J. and Coombs, M.G., "Advanced Heat Receiver Conceptual Design Study", Journal, N88-
- , Lewis Research Center, 1988.
- Zhao yu-xin., "Tutorial of Fluent (M)", Aerospace Institute, National Defence University of Science and
- Technology, 2003.
- Hitoshi, N., Tsutomu, F. and Takeshi, H., "An Experimental Study of a Solar Receiver for JEM Experiment Program", AIAA-2000-2996.
References
Dennis Alexander., "2KV Solar Dynamic Ground Test Demonstration Project", Report. NASA-CR198423, Tempe. Arizona, Allied Signal Aerospace, 1997.
"Solar Dynamic Power System Development for Space Station Freedom", Report. NASA-RP-1310, N94-12807, Cleveland, Ohio, Lewis Research Center, 1993.
Hal J. Strumpf., "On-Orbit Performance Prediction of the Heat Receiver for the U.S/Russia Solar Dynamic Power Flight Experiment", Journal. IEEE, 1996.
Marvin Warshay and Thaddeus Smog., "The NASA Advanced Solar Dynamic Technology Program", IEEE, 1989.
Roger A Crane., "Thermal Performance of Specific Heat Receiver Concepts for Advanced Solar Application", Report. IEEE, 1989.
Anthony, P., "Advanced Solar Brayton Space Power Systems", Report. IECEC Paper 899492.
Hal J. Strumpf and Chiristopher Krystkowiak., "Design of the Heat Receiver for the US/Russia Solar
Dynamic Power Joint Flight Demonstration", Report. IECEC Paper, 1995, pp.411-416.
Strumpf, H.J. and Coombs, M.G., "Advanced Heat Receiver Conceptual Design Study", Journal, N88-
, Lewis Research Center, 1988.
Zhao yu-xin., "Tutorial of Fluent (M)", Aerospace Institute, National Defence University of Science and
Technology, 2003.
Hitoshi, N., Tsutomu, F. and Takeshi, H., "An Experimental Study of a Solar Receiver for JEM Experiment Program", AIAA-2000-2996.