Transition measurement for the nature-laminar wing based on TSP technique

WU Ning; TANG Xin; DUAN Zhuoyi; ZHANG Yanjun

doi:10.11729/syltlx20190085

Volume 34 Issue 6

Dec. 2020

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Article Navigation > Journal of Experiments in Fluid Mechanics > 2020 > 34(6): 66-70

WU Ning, TANG Xin, DUAN Zhuoyi, et al. Transition measurement for the nature-laminar wing based on TSP technique[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(6): 66-70. doi: 10.11729/syltlx20190085

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Transition measurement for the nature-laminar wing based on TSP technique

doi: 10.11729/syltlx20190085

The First Aircraft Institute of AVIC, Xi'an 710089, China

Received Date: 2019-07-02
Rev Recd Date: 2019-11-11
Publish Date: 2020-12-25

Abstract

Abstract

In order to verify the design results of a laminar flow wing, a high-speed wind tunnel test was carried out in the DNW-HST wind tunnel in the Netherlands, and the transition position of the boundary layer on the wing surface was measured by the TSP method in the test. The experimental results show that the TSP method is very effective in detecting the transition position of the natural laminar airfoil surface. At the same time, it is found that the test has high requirements on the surface finish of the wing, and the test results are very sensitive to the surface pollution of the wing.
- nature-laminar wing,
- wing tunnel test,
- Temperature-Sensitive Paint(TSP),
- transition

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References(18)

References

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