Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method
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Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method
Vol. 25, Issue 10, (2010)
作者机构:
北京航空航天大学 能源与动力工程学院航空发动机数值仿真研究中心,北京,100191
作者简介:
基金信息:
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Published:2010
稿件说明:
移动端阅览
LIU Jian-ming, JIANG Xiang-hua, QIN Yin-lei, et al. Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method[J]. 2010, 25(10).
DOI:
LIU Jian-ming, JIANG Xiang-hua, QIN Yin-lei, et al. Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method[J]. 2010, 25(10).DOI:
Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method
In view of the shortages of current fluid-solid coupling arithmetic in simulating the failure of solid-element structures
fluid-solid coupling numerical simulation methods of solid-element flat blade were studied and validated with MSC.Dytran software while considering its integrity and failure.On this basis
in combination with very common and serious bird impact accidents in the working process of high bypass ratio aero-engines
Finite element method(FEM) model of the solid-element hollow blades with transient dynamic load for bird impact was established and the corresponding calculation was performed.Result shows that
huge instantaneous impact stresses will occur in the blades after bird strike
leading to local plastic deformation of the blades.The failure process of the blades after bird strike was simulated finally.