|
|
|
| Correction Technique of Spacecraft Thermal Network Model on the basis of Node Group Combined Method |
| (School of Mechanical Engineering , Shanghai Jiaotong University, Shanghai 200240, China) |
|
|
|
|
Abstract On the basis of the component of node thermal network equation in spacecraft and combining design feature of actual mechanism, a parametric node group thermal network combined equation whose physical meaning is definite was established and the correction technique of thermal network model for spacecraft was made on this basis. The extrapolated formula for calculating temperature that is based upon hot tests and basic principle of heat transfer can be used for determining those node temperature on which there are not measuring points, so the difficult subject is solved that measuring point in temperature is not enough during hot test and the model correction can not be put into effect. Using this correction model, calculating values whose errors are in permissible range can be conducted.
|
|
Published: 29 June 2011
|
|
|
|
|
|
| [1] |
WANG Cai-Li, DENG Dong, LI Yang, WANG Rong-Shun. Experimental Study on Influencing Factors and Their Effects on No-Vent Fills[J]. J. Shanghai Jiaotong Univ.(Sci.) , 2011, 45(09): 1400-1405. |
| [2] |
ZHUANG Da-Wei-1, PENG Hao-2, HU Hai-Tao-1, DING Guo-Liang-1, ZHU Yu-1. Nucleate Pool Boiling Heat Transfer Characteristics of Refrigerant/Oil Mixture with Diamond Nanoparticles[J]. J. Shanghai Jiaotong Univ.(Sci.) , 2011, 45(06): 861-865. |
| [3] |
LIU Zhen-Hua, YANG Xue-Fei. Boiling Heat Transfer Characteristics of Nanofluids in a Thermosyphon Loop[J]. J. Shanghai Jiaotong Univ.(Sci.) , 2011, 45(06): 890-894. |
|
|
|
|
