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BALLISIIC AND AIRDYNAMICS

Development and Application of a Novel Four Components Plate Type Hinge Moment Balance

  • PAN Huaye ,
  • ZHANG Qingchuan ,
  • WANG Shumin
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  • 1 Department of Modern Mechanics, University of Science and Technology of China, Hefei 230027, China
    2 China Aerodynamics Research and Development Centre, Sichuan Mianyang 621000, China

Received date: 2014-03-30

  Online published: 2025-05-26

Abstract

By the limitation of the testing model and balance structure, wind tunnel balance's precision and accuracy is lower, and it's hard to measure axial force of the control flap in high wind tunnel testing, so the quality of the testing data can be influenced. For solving this question, multi-beam symmetrical structure and a new combined bridge scheme had been designed, finally, a novel four components plate type hinge moment balance had been completed, which can measure axial force efficacious and was used in certain airplane model control flap hinge moment testing successfully. The calibration results and the test data shows that the balance's precision and the accuracy is better than normal three components plate type hinge moment balance, use such type of balance can increase the quality of the testing data efficiently which has good application value.

Cite this article

PAN Huaye , ZHANG Qingchuan , WANG Shumin . Development and Application of a Novel Four Components Plate Type Hinge Moment Balance[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(2) : 129 -133 . DOI: 10.15892/j.cnki.djzdxb.2015.02.033

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References

[1]
王发祥. 高速风洞实验[M]. 北京: 国防工业出版社, 2003.
[2]
李周复. 风洞特种试验技术[M]. 北京: 航空工业出版社, 2010.
[3]
熊琳, 刘展, 陈河梧. 舵面天平技术及其在高超声速风洞的应用研究[J]. 实验流体力学, 2007, 21(3):55-57.
[4]
刘喜贺, 王天昊, 邱俊文, 等. 四分量片式铰链力矩天平技术及风洞实验应用研究[J]. 实验流体力学, 2011, 25(2):88-91.
[5]
陈丽, 赵协和, 刘维亮, 等. 提高测量最大铰链力矩试验数据精准度的有效模拟技术研究[J]. 流体力学实验与测量, 2002, 16(3):51-56.
[6]
彭云, 谢新跃. 虚拟样机与天平研制[J]. 流体力学实验与测量, 2004, 18(3):83-87.
[7]
孔德永, 吴桂馥. 舵面铰链力矩的估算[J]. 空气动力学学报, 2005, 23(2):263-266.
[8]
白静, 解亚军. 风洞翼型天平校准技术[J]. 弹箭与制导学报, 2011, 31(6):169-172.
[9]
贺德馨. 风洞天平[M]. 北京: 国防工业出版社, 2002.
[10]
张平, 赵长辉, 刘博宇. 套筒式张线天平研制[J]. 实验流体力学, 2012, 26(4):101-104.
Outlines

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