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Temperature control and simulation of helicopter's sand/dust environmental test tunnel

  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

The change range of heat load in helicopter's sand/dust test tunnel is so wide that different heat balance devices are needed for high and low heat loads, and that the temperature control is difficult. In order to solve the temperature control problem more simply, a temperature control strategy with wind speed corresponding factor is presented based on the dynamic analysis and modeling of tunnel's temperature change. Simulation results show that this control strategy can manage the cooling and heating devices on different load conditions and temperature in tunnel is controlled at demand point successfully.

源语言英语
页(从-至)135-138
页数4
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
26
2
出版状态已出版 - 3月 2005

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