1.
Cracking Resistance Analysis of Complex Binder Pastes in Early Age
早龄期复合胶凝材料的裂纹扩展阻力分析
2.
The modified tensile stress crack propagation criterion and influence of cranny hydraulic pressure on crack propagation
修正的拉应力裂纹扩展准则及裂隙水压对裂纹扩展的影响
3.
Initally 24 mm holes were drilled at the crack tips to arrest propagation.
最初，在裂纹尖端钻24mm的孔以阻止其扩展。
4.
Study on Fatigue Crack Propagation Behavior of a New Burn Resistant Titanium Alloy-Ti40 Alloy;
Ti40新型阻燃钛合金疲劳裂纹扩展行为研究
5.
Fatigue crack growth probability model based on stress ratio
考虑应力比的疲劳裂纹扩展概率模型
6.
Study on random wave force spectrum and structural fatigue cracking propagation
随机波浪力谱及结构件裂纹扩展研究
7.
Based on the boundary Variational theorem, the energy release quantity and energy release rate (dynamical crack extension force) along the crack bounndary are obtained.
由此可以求得动态裂纹扩展时,沿裂纹边界的能量释放量和能量释放率(动态纹裂扩展力)。
8.
fracture mechanics can be used to determine the conditions in which a rapidly propagating crack can be arrested
断裂力学可用来确定制止裂纹快速扩展的条件。
9.
Hydraulic Fracture Test and Crack Propagation Simulation by Element-Free Method;
岩体水力劈裂试验及裂纹扩展的无单元法计算
10.
Influence of Ce on Crack Closure Effect and Intrinsic Fatigve CrackGrowth Resistance In Al-Li Alloy
铈对铝锂合金裂纹闭合效应及本征疲劳裂纹扩展抗力的影响
11.
Crack defect promotes crack initiation and growth.
裂纹缺陷促进了裂纹的萌生和扩展.
12.
initiation of stable crack growth
稳态裂纹扩展的开始
13.
The Research of J～* Integral in Elastic-Plastic Fracture Mechanics and Fracture Criterion for Mixed Mode Crack Propagation;
弹塑性断裂力学之J～*积分与复合型裂纹扩展断裂准则的研究
14.
The fatigue testing of the heterogeneous plates showed that the mechanical heterogeneity affected the fatigue crack growth rate.
试验表明,力学不均匀性影响疲劳裂纹扩展速率。
15.
Anisotropic Plastic Stress Fields at a Slowly Propagating Crack Tip
缓慢扩展裂纹尖端的各向异性塑性应力场
16.
Chaotic Analysis on Extended State of Crack in Brittle Rock;
脆性岩石裂纹尖端扩展状态的混沌动力学分析
17.
Study on Fatigue Crack Propagation and Stress Intensity Factor of Surface Cracks;
表面裂纹疲劳扩展和应力强度因子研究
18.
FATIGUE INTERFACIAL CRACK GROWTH BEHAVIOR ON THE RC BEAMS STRENGTHENED WITH PRESTRESSED FRP
预应力FRP加固RC梁的界面疲劳裂纹扩展规律