Design and Application of an all Moving Wing Model Limiting and Locking Device

Bo Lu; Bin Bin Lv; Li Yu; Hong Tao Guo; Yu Yan; Xi Ping Kou

doi:10.4028/www.scientific.net/AMR.753-755.1031

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 753-755Design and Application of an all Moving Wing Model...

Design and Application of an all Moving Wing Model Limiting and Locking Device

Abstract:

To effectively excite the all moving wing flutter model and limiting or quick locking model in case of bigger amplitude of the model, an excitation and limiting and locking device is designed for the high-speed wind tunnel flutter test model. This paper introduces the structure arrangement, control principle and strategy of this device. The wind tunnel flutter test indicates that this device can enhance the SNR of the test data, improve the boundary prediction precision of flutter, prevent the model from entering the flutter divergence state and protect the model and wind tunnel test equipment.

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Periodical:

Advanced Materials Research (Volumes 753-755)

Pages:

1031-1034

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.753-755.1031

Citation:

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Online since:

August 2013

Authors:

Bo Lu, Bin Bin Lv, Li Yu, Hong Tao Guo, Yu Yan, Xi Ping Kou

Keywords:

Flutter, Flutter Model, Limiting and Locking Device, Wind Tunnel Test

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References

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