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Topology Optimization of Frame of Aircraft Deicing Vehicle under Multiple Loading Conditions Based on Ansys
Abstract:
Firstly this article briefly describes the technology of topology optimization. Then the design space of frame of aircraft deicing vehicle is established and the model of finite element is gained by meshing. Loads and DOF constraints are applied based on the analysis of working conditions. The results of topology optimization are attained by calculation. On the basis of aforementioned results, the analysis is made. Finally, this paper makes a summary and outlook.
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2006-2009
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September 2013
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© 2013 Trans Tech Publications Ltd. All Rights Reserved
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