The Effect of Attack Angle on the Performance of Wave Glider Wings

Bing Huan Zheng; Chun Ying Xu; Chao Ling Yao; Jia Wang Chen

doi:10.4028/www.scientific.net/AMM.727-728.587

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 727-728The Effect of Attack Angle on the Performance of...

The Effect of Attack Angle on the Performance of Wave Glider Wings

Abstract:

In this paper, on the basis of static stress analysis of the Glider wings, we compare different factors influencing the drag force converted by the glider wings and optimize them by comparing the simulation results with the calculation results. The results shows that the horizontal component force is reach maximum value when attack angle reaches 45°. After that the horizontal component force decreases as attack angle increases. The horizontal component force is gradually increased as the flow rate increases under same attack angle.

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Periodical:

Applied Mechanics and Materials (Volumes 727-728)

Pages:

587-591

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.727-728.587

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Online since:

January 2015

Authors:

Bing Huan Zheng, Chun Ying Xu, Chao Ling Yao, Jia Wang Chen*

Keywords:

Catamaran Structure, Glider, Kinetic Model, Water Vehicles, Wave Glider

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* - Corresponding Author

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