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Keywords: Engine components
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Journal Articles
The multidisciplinary design optimization method of aero engine fan blade based on the airworthiness compliance and approximation model
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Multidiscipline Modeling in Materials and Structures (2013) 9 (2): 177–184.
Published: 09 August 2013
... of fan blade. The software of Isight was utilized to carry out the optimization. Haijun Zeng can be contacted at: zhjnuaa@163.com © Emerald Group Publishing Limited 2013 Aero engine Airworthiness Fan blade Approximation model Aircraft engines Engine components Among...
