首页> 外文会议>Fifth International Conference on Durability Analysis of Composite Systems, Nov 6-9, 2001, Tokyo, Japan >Methodology for predictable damage growth design of aircraft composite structures
【24h】

Methodology for predictable damage growth design of aircraft composite structures

机译:飞机复合材料结构可预测的损伤增长设计方法

获取原文
获取原文并翻译 | 示例

摘要

(1) The purposes of PDGD are improvement of design allowables and realization of additional weight saving needs for new aircraft and maintaining flight safety of aging aircraft. (2) Many current comprehensive studies to characterize the complicated phenomena concerned about fracture mechanics of composite materials lead to the construction of methodology for PDGD.
机译:(1)PDGD的目的是改善设计允许范围,并实现新飞机减轻额外重量的需求,并保持老化飞机的飞行安全性。 (2)目前许多有关表征复合材料断裂力学的复杂现象的综合研究导致PDGD方法的构建。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号