说明:双击或选中下面任意单词,将显示该词的音标、读音、翻译等;选中中文或多个词,将显示翻译。
您的位置:首页 -> 句库 -> 损伤容限设计
1.
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
2.
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
3.
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
4.
Aircraft Design Integration Discussion for Improved Damage Tolerance
增强飞机损伤容限的设计一体化探讨
5.
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。
6.
Structural Design and Damage Identification of Filament-Wound Toroidal Vessels;
纤维缠绕环形容器结构设计与损伤检测
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.
Analysis of Effect of Design Transients and Fatigue Damage on RPV Design Life
设计瞬态和疲劳损伤对反应堆压力容器设计寿命的影响分析
9.
Investigation of Design Criterion and Welding Repair Principle of High Temperature Components Using Continuum Damage Mechanics Based Finite Element Method;
连续损伤力学有限元法在高温构件设计和焊接修复中的应用
10.
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
11.
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
12.
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
13.
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
14.
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
15.
Experimental device for inducing diffuse brain injury in small animals
小动物弥漫性脑损伤致伤装置的设计
16.
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。
17.
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
18.
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