creep buckling and elastic-plastic buckling of stiffened cylindrical shells under pure bending

the analysis of creep buckling of compressed column with initial imperfection and torsional elastic restraint

具初始缺陷两端扭转弹性约束压杆的蠕变屈曲分析

creep buckling of circular shells under axial compression

圆柱壳体的轴压蠕变屈曲

characteristics of creep buckling for viscoelastic laminated plates

黏弹性结构蠕变屈曲特性的分析

the effect of the difference boundary conditions, initial imperfection and load on creep buckling are discussed.

讨论了不同边界条件、初始缺陷及载荷对压杆蠕变屈曲的影响。

creep buckling of columns under nonuniform temperature distribution

非均匀温度场压杆蠕变屈曲分析

a solution of creep buckling of finitely long cylindrical shells at external pressure

有限长圆柱壳外压蠕变屈曲解

a study of contact thermo-elasto-plastic creep buckling

接触热弹塑性蠕变屈曲研究

experimental investigation of creep buckling of thin wall cylindrical shells under external pressure at high temperature

高温外压下薄壁筒蠕变屈曲实验研究

using the sandwich model to analyze the creep buckling of compressed columns

采用夹层模型对压杆蠕变屈曲问题的分析

in creep buckling analysis, a ratio stress-strain method is proposed.

在蠕变分析中，本文提出了比应力-应变方法。

a mach number flutter trend of a typical airfoil section with a control surface is analyzed and the results obtained agree well with those with cfd/ csd direct coupling method.

分析了典型三自由度二元机翼的颤振边界，分析结果与CFD/CSD直接耦合方法吻合。

the numerical simulation of the flow around the rudder with naca airfoil section and the computer aided design of the semi-spade rudder

NACA半悬挂舵舵叶流场数值模拟及舵装置辅助设计

this dissertation presents how to use the ultrasonic motor as an actuator to suppress the flutter of a two-dimensional airfoil section with a control surface.

本研究旨在尝试通过超声电机驱动的控制面来实现二维翼段颤振的主动抑制。

this paper shows the wind tunnel testing results of naca four symmetrical airfoil section cascades of wells turbine for wave energy conversion.

本文介绍用于波能转换的威尔斯涡轮的NACA四位数对称叶型叶栅的风洞试验结果。

a polynomial fitting approach is presented, and thus the key question of fitting smooth blade surface from limited airfoil section is solved.

提出了多项式拟合方法，解决了由有限翼型截面拟合光滑叶片表面的关键问题。

the interference effects of support system of airfoil section ventral strut and sting on complete aircraft model with large aspect ratio and its components

翼型叶片腹支／尾支对大飞机全机及部件的干扰&大飞机全模试验技术及支撑干扰研究之三

for aeroservoelasticity of an airfoil section, this paper mainly considers with time delayed feedback control.

随后，针对二元机翼进行了气动伺服弹性研究，主要集中在反馈控制以及延迟反馈控制对气动弹性稳定性的影响。

experimental investigation on flow field around blade-tip airfoil section of horizontal-axis wind turbine

水平轴风力机叶尖翼型截面流场的试验研究

the interference effects of support system combination of airfoil section ventral strut and sting

低速风洞尾撑支杆干扰研究翼型叶片腹支－尾支组合支撑的干扰特性

two test methods, natural radioactive background method and decay method, used to verify the detection limit of radioactive aerosol monitors are studied.

研究了放射性气溶胶监测仪的检测方法，即天然本底检测法和衰变检测法。