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飞机结冰过程的液/固相变传热研究 被引量:4

Investigation on liquid/solid phase change heat transfer of aircraft icing
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摘要 基于液/固相变的基本理论,对飞机结冰过程的液/固相变传热特性进行了研究,建立了液膜及冰层生长的分析模型,并采用该模型对来流条件各参数对冰层生长特征及其速率的影响进行了分析.研究表明,在飞机结冰过程中,冰层生长速率及不同冰型的形成不但受来流参数的影响,而且与固、液相区的内部传热特性相关,因而考虑各相区的传热过程是提高冰层生长预测准确性的重要途径.所建模型考虑了液/固相变的非线性特征,对冰层生长速率及冰型特征有着较好的预测作用. The liquid/solid phase change heat transfer characteristics of aircraft icing were investigated based on the theories of liquid-solid phase change.The analysis model for the growth of film and ice was established and the influence of airflow parameters on the characteristics and rate of icing accretion was analyzed.The results indicate that the accretion rate of icing is not only influenced by the airflow parameters but also influenced by the inner heat transfer of each phase.The heat transfer in solid and ...
出处 《航空动力学报》 EI CAS CSCD 北大核心 2009年第8期1824-1830,共7页 Journal of Aerospace Power
基金 国家自然科学基金(10672174) 中国博士后科学基金(20080430230)
关键词 飞机 结冰 相变 传热 aircraft icing phase change heat transfer
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参考文献6

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同被引文献46

  • 1陈维建,张大林.飞机机翼结冰过程的数值模拟[J].航空动力学报,2005,20(6):1010-1017. 被引量:25
  • 2Icing Wind Tunnel Interfacility Comparison Tests [S]. AIR5666-2012-10-03.
  • 3Thomas B. Irvine, John R. Oldenburg, David W. Sheldon. The New Icing Cloud Simulation System at NASA LEWIS' Icing Research Tunnel[J]. AIAA 1997.
  • 4Chirag Bhargava, Eric Loth. Simulating the Aerodynamics of the NASA John H. Glenn Icing Research Tunnel[J]. Journal of Aircraft, Vol. 42. No. 3, May-June 2005.
  • 5Edward Herman. Goodrich Icing Wind Tunnel Overview hn- provements and Capabilities [J]. A IA A 9-12, Jan 2006.
  • 6Peter Struk, Tom Currie, William Benjamin Wright, Daniel C. Knezevici, Dan Fuleki, Andy Broeren, Mario Vargas, Jen- Ching Tsao. Fundamental Ice Crystal Accretion Physics Studies [J]. SAE International, 2011-38-0018.
  • 7Richard K. Jeck. Calibration and Use of Goodrich Model 0871FA Ice Detectors in Icing Wind Tunnels[J]. Journal of Aircraft, Vol. 44, No. 1, Jan-Feb 2007.
  • 8Andy P. Broeren, Sam Lee, Gautam H. Shah, Patrick C. Murphy. Aerodynamic Effects of Simulated Ice Accretion on a Generic Transport Model [J]. SAE International 2011- 38 -0065.
  • 9Olsen, W. , Takeuchi, D., and Adams, K.. Experimental Comparison of Icing Cloud Instruments [J]. AIAA 83 - 0026, Jan. 1983.
  • 10Cebeci T, Kafyeke F. Aircraft icing[J]. Annual Review of Fluid Mechanics, 2003, 35:11-21.

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