[1] 武淮生,钟群鹏. 飞机发动机零部件结构完整性的概率R6评定. 航空学报,2000,21(4): 96-99.
[2] 吴德锋,隋福成,毛春见. 先进飞机典型结构关键部位损伤容限分析研究. 飞机设计,2010(10): 16-19.
[3] R6. Assessment of the integrity of structures containing defects, Revision 3. British Energy Generation, 2000.
[4] BS7910. Guide to methods for assessing the acceptability of flaws in metallic structures. London, BSI, 2005.
[5] FITNET. Fitness for service analysis of structures using the FITNET procedure; An Overview, 24th Int. Conf. on Offshore Mechanics and Artic Eng., Greece 12-17 June, 2005.
[6] API RP 579. Standardized fitness-for-service assessment techniques for pressurized equipment used indthe petroleum industry. API, 2004.
[7] 钟群鹏,李培宁. 国家标准《在用含缺陷压力容器安全评定》的特色和创新点综述. 管道技术与设备,2006(1): 1-5.
[8] ASTM E399-09. Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness KIC of Metallic Materials, ASTM, 2002.
[9] BS7448-1. Fracture mechanics toughness tests-Method for determination of KIC, critical CTOD and critical J values of metallic materials. BSI, 1991.
[10] GB/T 2358-94, 金属材料裂纹尖端张开位移试验方法.
2012, 
