Foam-Core Effect on the Integrity of Tailplane Leading Edge During Bird-Strike Event

被引：24

作者：

Hedayati, Reza ^{[1
]}

Ziaei-Rad, Saeed ^{[1
]}

机构：

[1] Isfahan Univ Technol, Dept Mech Engn, Esfahan 8415683111, Iran

来源：

JOURNAL OF AIRCRAFT | 2011年 / 48卷 / 06期

关键词：

AIRCRAFT; IMPACT;

D O I：

10.2514/1.C031451

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The objective of this paper is to describe the procedure of optimizing the leading-edge structure of a tailplane in an industrial environment. The paper also investigates the effect of implementing a foam core between aluminum sheets in a tailplane leading-edge structure. Bird strike against two types of leading-edge structures, one with and the other without a foam core, was investigated and then the optimum design for each case was determined. The results indicate that if a foam core is embedded between the aluminum sheets instead of increasing the thicknesses of aluminum sheets, the skin overall weight can be reduced by 32%.

引用

页码：2080 / 2089

页数：10

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