AEROELASTIC TAILORING OF A WING WITH COMPOSITE SKIN

被引：0

作者：

Guan De and Zhong Ke Beijing University of Aeronautics and Astronautics

机构：

来源：

Chinese Journal of Aeronautics | 1989年 / 04期

关键词：

link; AEROELASTIC TAILORING OF A WING WITH COMPOSITE SKIN;

D O I：

暂无

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学科分类号：

摘要：

<正> Preliminary results of aeroelastic tailoring of a wing of medium aspect ratio,medium sweptback angle constructed with composite skin and metal frames arepresented. The composite skin is modeled with quadrilateral plates of orthotropicmaterial. Tsai-Hill failure theory is used in fully stressed design of the compositeskin, and uniform derivative criteria are used in the optimization with respect toflutter speed and aileron effectiveness. Preliminary results indicate the feasibility ofthe method, and reasonable results are achieved by a few steps of redesign.

引用

页码：271 / 276

页数：6