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 USSR 9
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 Service 31
飞机结构的损伤容限 38
Operational Damage Tolerance of Airframe 47
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 Aircraft 69
用解析法和实验法确定机体载荷 73
Analytical and Experimental Evaluation of Airframe Loads 84
飞机结构耐久性设计 88
A Methodology of durability Design for Aircraft Structures 104
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 Design 121
飞机结构高温寿命研究 125
Elevated Temperature Life Research for Aircraft Structures 132
三阶段疲劳全寿命估算模型 138
Three Stages Model for Predicting Total Fatigue Life 143
典型结构件的全寿命预测 147
The Total Fatigue Life Prediction for Typical Structure Components 157
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 Prediction 171
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 Compressor 187
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 Tunnel 214
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 Concept 244
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 Type 270