1.
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。
2.
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。
3.
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
4.
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
5.
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
6.
Research on Strain Fatigue Characteristics of Pressure Vessel Steel 16MnR after High Temperature Damage;
压力容器用钢16MnR高温损伤后应变疲劳特性研究
7.
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
8.
Vibration Characteristic Research of Stochastic Damaged Stiffened Panel Based on Monte Carlo Stochastic FEM;
基于Monte Carlo法结构随机损伤有限元动力特性研究
9.
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
10.
Aircraft Design Integration Discussion for Improved Damage Tolerance
增强飞机损伤容限的设计一体化探讨
11.
Analysis of Concrete Damage Mechanism and Critical Damage Characteristics;
混凝土损伤机理及临界损伤特性分析
12.
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
13.
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
14.
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
15.
Dynamic Behaviors and Damage Identification of Structures;
具有分布损伤的结构动特性及其损伤识别
16.
Vibrational Power Flow Characteristics of Cracked Structures and the Damage Detection;
裂纹损伤结构的振动功率流特性与损伤识别
17.
Study on the characteristics of violence injury in 734 injured individuals in Chongqing;
重庆市734例暴力性伤害案伤者损伤特征分析
18.
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