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Measuring Technique for Micro Rolling Moment in Wind Tunnel Tests

  • LIU Gaoji ,
  • YU Weiqing ,
  • WANG Chen
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  • 1 Xi'an Modern Control Technology Research Institute, Xi'an 710065, China
    2 Shenyang Aerodynamics Research Institute, Aviation Industry Corporation of China, Shenyang 110034, China

Received date: 2017-12-20

  Online published: 2025-05-30

Abstract

the problem of low measurement precision in measuring micro rolling moment in wind tunnel tests of spinning projectiles is solved, this paper proposes a new type of structural configuration that some gauges are placed inside the model as the internal elements and some gauges are put outside the model as the external elements to minimize the interaction between the force components. The paper performs the design optimization of strain-gauge balance and conducts sensitivity design with finite-element method, successfully developing a set of new-type strain-gauge balance for measuring micro rolling moment in wind tunnel for force measurement tests. The static calibration precision of the balance satisfies the indices stipulated in the national military standard GJB2244A-2011 for strain-gauge balance in wind tunnel tests, the dynamic calibration precision of rolling moment component reaches the advanced index of the Precision Criterion for Calibration Model of Projectile-like Weapons in Wind Tunnel Force Measurement Tests, improving the precision of wind tunnel force measurement for spinning projectiles.

Cite this article

LIU Gaoji , YU Weiqing , WANG Chen . Measuring Technique for Micro Rolling Moment in Wind Tunnel Tests[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018 , 38(4) : 104 -108 . DOI: 10.15892/j.cnki.djzdxb.2018.04.025

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References

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[2]
中国人民解放军总装备部 GJB 2244A-2011 风洞应变天平规范. 北京: 总装备部军标出版发行部, 2011: 10-19.
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范洁川 风洞试验手册 北京: 航空工业出版社, 2002: 184-200.
Outlines

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