首页 | 本学科首页   官方微博 | 高级检索  
     检索      

气动弹性剪裁中的设计变量和约束导数
引用本文:高萍,张芝龙.气动弹性剪裁中的设计变量和约束导数[J].航空学报,1991,12(12):647-650.
作者姓名:高萍  张芝龙
作者单位:北京航空航天大学 (高萍),北京航空航天大学(张芝龙)
摘    要:1.前言 设计变量的取法和约束导数的计算,不但影响气动弹性剪裁的结果,而且决定着它的工作量。本文对于两种不同的设计变量取法进行了讨论。在约束导数计算方面,通过一个盒段模型和一个三角翼模型的计算,进行了对比。

关 键 词:气动弹性  复合材料  结构优化  

DESIGN VARIABLES AND CONSTRAINT DERIVATIVES IN AEROELASTIC TAILORING
Beijng University of Aeronautics and Astronautics Gao Ping and Zhang Zhilong.DESIGN VARIABLES AND CONSTRAINT DERIVATIVES IN AEROELASTIC TAILORING[J].Acta Aeronautica et Astronautica Sinica,1991,12(12):647-650.
Authors:Beijng University of Aeronautics and Astronautics Gao Ping and Zhang Zhilong
Institution:Beijng University of Aeronautics and Astronautics Gao Ping and Zhang Zhilong
Abstract:Two important point in aeroelastic tailoring, i.e., determination of design variables and calculation of constraint derivatives were discussed. Two different methods in the determination of the design variables were evaluated. It seems that the polynomial expression of the thickness of the composite ply of the skin is more beneficial in practical application. By use of a simple box model and a delta wing model, the calculation of the derivatives of normal frequencies, mode shapes as well as flutter speeds are performed. Derivatives of normal frequencies and mode shapes calculated by stiffness and flexibility methods are all reasonable. In the calculation of the derivatives of flutter speeds, the effect of mode shape can be neglected.
Keywords:aeroelasticity  composite material  structural optimization  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号