Assessment of dynamic effects on aircraft design loads: The landing impact case

被引：8

作者：

Bronstein, Michael ^{[1
]}

Feldman, Esther ^{[1
]}

Vescovini, Riccardo ^{[2
]}

Bisagni, Chiara ^{[2
]}

机构：

[1] Israel Aircraft Ind Ltd, Tel Aviv, Israel

[2] Politecn Milan, Dept Aerosp Sci & Technol, I-20133 Milan, Italy

来源：

PROGRESS IN AEROSPACE SCIENCES | 2015年 / 78卷

关键词：

Design loads; Dynamic simulation; Aircraft design; Damping;

D O I：

10.1016/j.paerosci.2015.06.003

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper addresses the potential benefits due to a fully dynamic approach to determine the design loads of a mid-size business jet. The study is conducted by considering the fuselage midsection of the DAEDALOS aircraft model with landing impact conditions. The comparison is presented in terms of stress levels between the novel dynamic approach and the standard design practice based on the use of equivalent static loads. The results illustrate that a slight reduction of the load levels can be achieved, but careful modeling of the damping level is needed. Guidelines for an improved load definition are discussed, and suggestions for future research activities are provided. (C) 2015 Elsevier Ltd. All rights reserved.

引用

收藏

页码：131 / 139

页数：9

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