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Volume 35 Issue 3
Mar.  2009
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Journal of Beijing University of Aeronautics and Astronautics  > 2009  >  35(3): 308-312.
Zhang Pengfei, Cheng Wei, Zhao Yuet al. Measure of reaction wheels disturbance considering coupling effect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(8): 948-952. (in Chinese)
Citation: Zhang Lizhen, Wang Xiaoming, Dong Sujun, et al. Calculation of thermal load and impact factor analysis for hypersonic vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(3): 308-312. (in Chinese)
shu

Calculation of thermal load and impact factor analysis for hypersonic vehicle

  • 1.

    School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. Chengdu Aircraft Design & Research Institute, Chengdu 610041, China

  • Received Date: 19 Mar 2008
  • Publish Date: 31 Mar 2009
    Abstract
  • Endothermal thermal protection system (TPS) and liquid N2 heat sink were chosen to calculate the characteristics of thermal control system (TCS) in hypersonic vehicle. The methods of radiation balance and double lumped parameter were adopted to obtain the thermodynamic model of adiabatic layer and cabin air temperature. Therefore, aeroheating, adiabatic layer heat transfer and cabin air temperature were decoupled. On the basis of flight profile of X-34 hypersonic vehicle, the thermal load of avionics bay was calculated. Besides, the influence of adiabatic layer, cooling gas velocity and liquid N2 amount on cabin air as well as the equipment temperature were analyzed. The results show that this method could get the response characteristics of heat transfer sections, which played an important part in the primary stage of hypersonic vehicle design.

     

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