Current Status of Flight Simulation Fatigue Crack Growth Concepts

机译：飞行模拟疲劳裂纹扩展概念的现状

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

The current status of flight simulation fatigue crack growth concepts is reviewed. Crack growth models and methods of crack growth prediction are compared with respect to applicability and limitations. Research areas for improvement of crack growth prediction are specified.

著录项

作者
Wanhill, R. J. H. ; Schijve, J.;
展开▼
作者单位

展开▼
年度 1988
页码 1-20
总页数 20
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Fatigue(Materials); Crack propagation; Flight simulation; Aluminum alloys; Aircraft; Predictions; Mathematical models;

机译：疲劳（材料）;裂纹扩展;飞行模拟;铝合金;飞机;预测;数学模型;

相似文献

外文文献
中文文献
专利

1. Effect of Overload on the Near-Threshold Fatigue Crack Growth Rate in a 2024-T3 Aluminum Alloy: II. Fatigue Crack Growth Simulation for Calculating the Fatigue Life under Alternating Loading [J] . A. N. Savkin, R. Sunder, A. V. Andronik, Russian Metallurgy(Metally) . 2019,第5期

机译：超负荷对2024-T3铝合金近阈值疲劳裂纹生长速率的影响：II。交替加载下计算疲劳寿命的疲劳裂纹增长模拟
2. Atomistic simulations of fatigue crack growth and the associated fatigue crack tip stress evolution in magnesium single crystals [J] . Tang T., Kim S., Jordon J.B., Computational Materials Science . 2011,第10期

机译：镁单晶疲劳裂纹扩展及其相关的疲劳裂纹尖端应力演化的原子模拟
3. Simulations of fatigue crack propagation in friction stir welds under flight loading conditions [J] . Tommaso Ghidini, Claudia Polese, Agostino Lanciotti, Materialpruefung: Werkstoffe und Bauteile, Forschung Prufung Anwendung . 2006,第7a8期

机译：飞行载荷条件下搅拌摩擦焊缝疲劳裂纹扩展的模拟
4. Corrosion fatigue crack growth of 7475 T7351 aluminum alloy under flight simulation loading [C] . A. Chemin, D. Spinelli, W. Bose Filho International Conference on Material and Component Performance under Variable Amplitude loading . 2015

机译：腐蚀疲劳裂纹7475 T7351铝合金的飞行模拟载荷
5. Fatigue Crack Growth in Complex Residual Stress Fields Due to Surface Treatment and Foreign Object Damage Under Simulated Flight Cycles [D] . Zabeen, Suraiya. 2012

机译：在模拟飞行周期下，由于表面处理和异物损坏，复杂残余应力场中的疲劳裂纹扩展
6. Application of a New Energy-Based ΔS* Crack Driving Force for Fatigue Crack Growth Rate Description [O] . Grzegorz Lesiuk 2019

机译：基于能量的新型ΔS*裂纹驱动力在疲劳裂纹扩展速率上的应用
7. Corrosion Fatigue Crack Growth of 7475 T7351 Aluminum Alloy under Flight Simulation Loading [O] . Chemin A., Spinelli D., Filho W. Bose, 2015

机译：飞行载荷作用下7475 T7351铝合金的腐蚀疲劳裂纹扩展
8. Influence of Starter Notches on Flight Simulation Fatigue Crack Growth [R] . Wanhill, R. J. H., Schra, L. 1995

机译：起动器缺口对飞行模拟疲劳裂纹扩展的影响

Current Status of Flight Simulation Fatigue Crack Growth Concepts

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅