首页> 美国政府科技报告 >Effect of Speed of Testing and Internal Heating on the Fatigue Behavior of Notched Specimens of Titanium and its Alloys

【24h】

Effect of Speed of Testing and Internal Heating on the Fatigue Behavior of Notched Specimens of Titanium and its Alloys

机译：试验速度和内部加热对缺口试样钛及其合金疲劳行为的影响

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

No abstract available.

著录项

作者
Kaufman, J. G.; Crum, R. G.; D'Appolonia, E.;
展开▼
作者单位

展开▼
年度 1954
页码 p.1-36
总页数 36
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Titanium alloys; Notch sensitivity; Fatigue(Mechanics); Failure(Mechanics); Fatigue tests(Mechanics); Cyclic tests; Heat treatment; Thermal properties; Stress concentration; Behavior; Velocity; Test methods;

机译：钛合金;缺口敏感性;疲劳（力学）;失效（力学）;疲劳试验（力学）;循环试验;热处理;热性能;应力集中;行为;速度;试验方法;

相似文献

外文文献
中文文献
专利

1. Kinking Behavior of S-N Curve for Ti6AI4V Alloy Notched Specimen Under a Load-Controlled High Cycle Fatigue Test [J] . Aye Thant Htoo, Yukio Miyashita, Yuichi Otsuka, Materials science forum . 2016,第期

机译：Ti6Al4V合金缺口试样在载荷控制的高周疲劳试验下的S-N曲线弯曲行为
2. High temperature fatigue tests of notched specimens made of titanium Grade 2 [J] . Gallo P., Berto F., Lazzarin P. Theoretical and Applied Fracture Mechanics . 2015,第Null期

机译：2级钛制缺口试样的高温疲劳试验
3. Prediction of multiaxial fatigue life for notched specimens of titanium alloy TC4 [J] . Wu Z. R., Hu X. T., Li Z. X., Journal of Mechanical Science and Technology . 2016,第5期

机译：TC4钛合金缺口试样的多轴疲劳寿命预测
4. EXPERIMENTAL INVESTIGATION OF MICROSTRUCTURAL EFFECT ON SHORT FATIGUE CRACK BEHAVIOUR OF NOTCHED α+β TITANIUM ALLOY SPECIMENS [C] . M. Benedetti, L. Bertini, V. Fontanari, International Fatigue Congress . 2002

机译：缺口α+β钛合金标本短疲劳裂纹行为的微观结构效应的实验研究
5. The role of casting defects in the fatigue behavior of notched cast aluminum alloys. [D] . Dabayeh, Ashraf A. 1998

机译：铸造缺陷在缺口铸造铝合金疲劳行为中的作用。
6. Effect of Low Cycle Fatigue Predamage on Very High Cycle Fatigue Behavior of TC21 Titanium Alloy [O] . Baohua Nie, Zihua Zhao, Yongzhong Ouyang, 2017

机译：低周疲劳预损伤对TC21钛合金超高周疲劳行为的影响
7. Fatigue Notch Sensitivity of Age-Hardened Aluminum Alloy in Rotating Bending Tests : Investigations Based on the Specimens Having an Extremely Small Notch [O] . Hitonobu NISHITANI, Masahiro ENDO 1984

机译：年龄硬化铝合金在旋转弯曲试验中的疲劳缺口敏感性：基于具有极小缺口的标本的研究
8. FATIGUE STRENGTHS OF AIRCRAFT MATERIALS AXIAL-LOAD FATIGUE TESTS ON EDGE-NOTCHED SHEET SPECIMENS OF 2024-T3 AND 7075-T6 ALUMINUM ALLOYS AND OF SAE 4130 STEEL WITH NOTCH RADⅡOF 0.004 AND 0.070 INCH [R] . H. J. Grover, W. S. Hyler, L. R. Jackson 1959

机译：2024-T3和7075-T6铝合金边缘板材以及saE 4130钢的轴向负荷疲劳试验的疲劳强度，缺口尺寸为0.004和0.070英寸

Effect of Speed of Testing and Internal Heating on the Fatigue Behavior of Notched Specimens of Titanium and its Alloys

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅