Volume 46 Issue 2
Feb.  2020
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TIAN Yongqiang, CAI Jinsheng, ZHANG Zhengke, et al. Similarity theory in icing wind tunnel test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(2): 359-370. doi: 10.13700/j.bh.1001-5965.2019.0340(in Chinese)
Citation: TIAN Yongqiang, CAI Jinsheng, ZHANG Zhengke, et al. Similarity theory in icing wind tunnel test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(2): 359-370. doi: 10.13700/j.bh.1001-5965.2019.0340(in Chinese)

Similarity theory in icing wind tunnel test

doi: 10.13700/j.bh.1001-5965.2019.0340
Funds:

National Natural Science Foundation of China 11472221

More Information
  • Corresponding author: CAI Jinsheng, E-mail: jcai@nwpu.edu.cn
  • Received Date: 28 Jun 2019
  • Accepted Date: 19 Aug 2019
  • Publish Date: 20 Feb 2020
  • Similarity is the basic requirements of all kinds of wind tunnel tests including icing wind tunnel tests. To systematically study the similarity problem of icing wind tunnel test, the in-flight icing problem is analyzed and summed up, and then the variables involved are summarized, including both their physical meanings and dimensions. Then some dimensionless variables are obtained by applying the similarity theory analysis method to the in-flight icing problem and the physical meanings of the dimensionless variables are analyzed. Some simplifications to the dimensionless variables of the in-flight icing problem are conducted by ignoring the unimportant factors, and then the dominant similarity parameters of icing wind tunnel tests are obtained. Finally, the method of selecting the operating parameters of the icing wind tunnel test on scale models is achieved by applying the similarity laws, it is verified by CFD and its feasibility is confirmed.

     

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