STRUCTURAL INTEGRITY IN AIRCRAFT.

被引:0
|
作者
Hardrath, H.F.
机构
关键词
D O I
暂无
中图分类号
学科分类号
摘要
The paper reviews briefly the current design philosophies for achieving long, efficient, and reliable service in aircraft structures. A research program is proposed, based on a computerized design scheme and correlating present knowledge on fatigue and fracture behavior. Objective is to optimize materials selection for maximum reliability between inspections.
引用
收藏
页码:3 / 12
相关论文
共 50 条