检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:王斐[1] 冉玉国[1] 李秋彦[1] WANG Fei;RAN Yuguo;LI Qiuyan(AVIC Chengdu Aircraft Design and Research Institute,Chengdu,Sichuan 610091,China)
机构地区:[1]航空工业成都飞机设计研究所,四川成都610091
出 处:《西南石油大学学报(自然科学版)》2021年第6期162-168,共7页Journal of Southwest Petroleum University(Science & Technology Edition)
摘 要:针对研制初期,飞机结构设计参数存在严重不确定性,颤振设计工作难以快速有效推进的问题,开展了方案设计阶段飞机颤振快速分析方法研究。采用虚拟质量法,通过在原结构一定位置施加虚拟质量,建立可覆盖局部结构参数变化的统一模态振型,然后将此虚拟质量从质量矩阵中移除,以防止影响原结构的动力学特性,并采用虚拟质量模态振型对不同参数下的质量矩阵、阻尼矩阵、刚度矩阵以及气动力矩阵进行广义化,建立虚拟质量模态空间下的颤振方程,并采用g法求解,得到不同参数下的飞机颤振速度。建立了一种飞机颤振快速分析方法,在面对大量参数开展敏感性研究分析时,能有效减少模态分析次数,提高飞机方案设计阶段分析效率。通过算例对比分析可知,该方法计算精度与传统方法基本一致,满足工程需求。Aiming at the difficulties in flutter design due to uncertainties of structural parameters for the initial stage of aircraft design project,the research on the aircraft flutter rapid analysis method in the planning stage is carried out.The fictitious mass method is applied to create a uniform mode shape that can cover the changes of local structural parameters.Then the fictitious mass is removed from the mass matrix to avoid affecting the dynamic characteristics of the original structure.The mass matrix,damping matrix,stiffness matrix and aerodynamic matrix under different parameters will be generalized with this mode shape.The flutter equation in the fictitious mass modal space is established,which is solved by the g method,and the flutter velocity of the aircraft with different parameters is obtained.In this paper,a fast analysis method of aircraft flutter is established,which can effectively reduce the work load of modal analysis and improve the efficiency of aircraft scheme phase analysis when carrying out sensitivity analysis in the face of a large number of parameters.Through the comparative analysis of examples,it can be seen that the calculation accuracy of this method is basically consistent with the traditional method,which meets the engineering needs.
分 类 号:V211.47[航空宇航科学与技术—航空宇航推进理论与工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.249