《国际科技合作课题论文集 4》

原苏联民航飞机结构强度要求的演变1

Evolution of the Civil Aircraft Structural Strength Requirements in the Former USSR9

对民用飞机使用环境及载荷的研究14

Investigation of External Effects and Loading of the Civil Aviation Aircraft in Service31

飞机结构的损伤容限38

Operational Damage Tolerance of Airframe47

提供老飞机结构完整性的方法和经验54

The Methodology and the Experience in Providing the Structural Integrity of Aging Aircraft69

用解析法和实验法确定机体载荷73

Analytical and Experimental Evaluation of Airframe Loads84

飞机结构耐久性设计88

A Methodology of durability Design for Aircraft Structures104

可靠性设计中的二维应力强度干涉模型116

Two Dimensional Stress-Strength Interference Model for Reliability-Based Design121

飞机结构高温寿命研究125

Elevated Temperature Life Research for Aircraft Structures132

三阶段疲劳全寿命估算模型138

Three Stages Model for Predicting Total Fatigue Life143

典型结构件的全寿命预测147

The Total Fatigue Life Prediction for Typical Structure Components157

局部应力应变法寿命计算中材料疲劳特性选用的评论165

Comment on the Option of Material Fatigue Characteristic Dascriptions in Local StresS-Strain Life Prediction171

非稳态效应对跨音速轴流压气机中测量的影响176

Influence of Unsteady Effects on the Measurements in a Transonie Axial Compressor187

在低速二元柔壁自适应壁风洞中的三元模型试验194

Testing of 3-D Models in a Low Speed 2-D Flexible Walled Wind Tunnel214

后缘分离机翼的气动力计算221

Computation of the Flow Around Wings With Rear Separation，Including the Curved Basic Flow Concept244

在不同类型风洞实验段中二元洞壁干扰的实验研究254

Experimental Investigation of 2-D Wall Interferences in Wind Tunnel Test Sections of Different Type270