Parameter Optimization of Nose Landing Gear Considering Both Take-off and Landing Performance of Ca

来源 :南京航空航天大学学报：英文版 | 被引量 : 0次 | 上传用户：lxm1230520

【摘要】

：

Optimization of the parameters of landing gear systems with double-stage air springs of catapult take-off carrier-based aircraft is here studied based on the ma

【作者】

：

Zhang Ming Nie Hong He Zhihang

【机构】

：

KeyLaboratoryofFundamentalScienceforNationalDefense-AdvancedDesignTechnologyofFlightVehicle,.StateKe

【出处】

：

南京航空航天大学学报：英文版

【发表日期】

：

2016年2期

【关键词】

：

carrier-based AIRCRAFT BUFFER PERFORMANCE fast-extension PERFORMANCE AIRCRAFT de

【基金项目】

：

supported by the National Natural Science Foundation of China(Nos.51305198,11372129)

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Optimization of the parameters of landing gear systems with double-stage air springs of catapult take-off carrier-based aircraft is here studied based on the mathematical equations of the classic dual mass spring-damper dynamic model.Certain standards for

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Parameter Optimization of Nose Landing Gear Considering Both Take-off and Landing Performance of Ca

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