1.
β-Grain Growth and Influence of Its Grain Size on Damage-Tolerance Property in Titanium Alloy
钛合金β晶粒生长规律及晶粒尺寸对损伤容限性能的影响
2.
Feasibility Study on Damage Tolerance Design of Titanium Alloys
钛合金结构损伤容限设计可行性研究
3.
The Assess on Safety Life、Durability and Damage Tolerance of Main Gear Strut Cylinder;
主起支柱外筒疲劳耐久性及损伤容限评估
4.
Synthetical Analysis of Durability and Damage Tolerance of Aircraft Structural Members under Corrosive Condition
腐蚀条件下飞机结构耐久性/损伤容限综合分析
5.
Damage Behavior of the Stiffened Plates Subjected to the Low-velocity Impact;
复合材料加筋板冲击损伤及损伤容限研究
6.
It not only improves damage tolerance behavior of composite structures, but also improves crack propagation properties of impact.
它不仅可用于改善结构在拉伸、切载荷下的损伤容限特性,同时也可提高蒙皮的抗冲击损伤特性。
7.
Study on Simulation for Ultimate Bearing Capacity of Oil-Derrick with Damage
考虑损伤的石油井架极限承载性能仿真研究
8.
Aircraft Design Integration Discussion for Improved Damage Tolerance
增强飞机损伤容限的设计一体化探讨
9.
The Study of Thermal-Mechanical Processing Technique of High Strength, High Toughness and Damage Tolerant Titanium Alloy;
高强高韧损伤容限钛合金热机械处理工艺研究
10.
A Study of Fatigue Crack Growth Rate of TC4-DT Titanium Lloy with Damage Tolerance;
损伤容限型TC4-DT钛合金疲劳裂纹扩展速率研究
11.
Study on the Damage Tolerance Methodology for the Wing Panel of New Regional Jet;
新支线飞机机翼下壁板损伤容限方法研究
12.
Low-modulus skin is an effective design method for improving damage tolerance behavior of composite structures.
低模量蒙皮设计概念是改进复合材料结构损伤容限特性的一种有效的设计方法。
13.
The Correlation between Chemoembolization Volume and Acute Liver Function Lesion after TACE in HCC;
TACE治疗原发性肝癌所致急性肝功能损伤与化疗栓塞容积的相关性研究
14.
An Orthogonal Anisotropic Ductile Damage Model Applicable to Deep- drawing Forming Limits
一种适用于成形极限的正交异性延性损伤模型
15.
Damage Tolerance Test and Methodology for the Lower Wing Panel Splicing of New Turbofan Jet;
新型涡扇飞机机翼下壁板对接件损伤容限试验和方法研究
16.
Dynamic Numerical Simulation and Damage Telerence Design of Torsion Bar under Random Load;
随机载荷下扭力轴动态响应的数值仿真分析和损伤容限设计
17.
Programming Method for Multi-crack Damage Tolerance Analysis of General Structures;
适用于新结构的多裂纹损伤容限分析程序实现方法
18.
OPTIMUM DESIGN BASED ON DAMAGE TOLERANCE FOR INTEGRATED WING-BEAM STRUCTURE
基于损伤容限设计思想的飞机整体翼梁优化设计