Study on Optimization Design of Flying Wing Layout Aircraft Considering the Effect of Propulsion Sys

来源 :Asian Congress of Structural and Multidisciplinary Optimizat | 被引量 : 0次 | 上传用户：zhongtuo97

【摘要】

：

【作者】

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Chuan-Yu Zheng Jiang-Tao Huang Yong-Gang Yu Zhu-Zhou

【机构】

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China Aerodynamics Research and Development Center, Building 278, Jianmen Street, Fucheng District,6

【出处】

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Asian Congress of Structural and Multidisciplinary Optimizat

【发表日期】

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2018年11期

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　　Conventional aircraft design is generally based on a clean configuration or ventilation model,which helps to reduce the complexity of the design object to speed up the optimization design process.However,due to the neglect of some structural and complex conditions,the optimization results in engineering can only be used in the preliminary rough design earlier.

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Study on Optimization Design of Flying Wing Layout Aircraft Considering the Effect of Propulsion Sys

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