Yangtao Yu

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To solve the performance changing problem of icing wing of one aircraft, a test method of aerodynamic characteristics and structural characteristics based on flow field and structure field coupled analysis is proposed. The method is used to discretely analyze time-averaged N-S equation of two-dimensional steady incompressible viscous flow by finite element(More)
Focusing on the On-Orbit Servicing technology, according to the design demand of mini-type universal automounous docking mechanism and using ADAMS-View software, the paper concluded the previous work in the following aspects: establishing a virtual prototype model of the mini-type universal docking organization and completing the dynamic characteristic(More)
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