Design and Thermal Simulation of the Airborne Missile Power Artificial Load
Received:March 11, 2016  Revised:August 15, 2016
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DOI:10.7643/ issn.1672-9242.2016.04.014
KeyWord:thermal analysis  thermal design  thermal simulation
     
AuthorInstitution
XU Lian-hu AVIC China Airborne Missile Academy, Luoyang, , China
DING Xin Aviation Industries Archives, Beijing,
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Abstract:
      Objective In order to select the optimal artificial load design plan. Methods Firstly the correlation between power and resistance was calculated for the power artificial load structure that was realized by power resistor. Two resistance plans were determined through the calculation. Then power artificial load was designed according to assessment requirements on airborne missile. Finally the optimal plan was chosen out through thermal simulation analysis. Results The thermal test evaluation was carried out for the artificial load which was made based on the selected plan. The deviation was no more than 2 ℃ between the results of thermal simulation and thermal test. Conclusion The data analysis indicates that the selected plan based on thermal simulation is reasonable and feasible.
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