This book provides a concise discussion of fatigue crack growth (FCG) failure and lifing analysis methods for metallic aircraft structures and components. After a reasonably concise historical review, surveys are made of (i) the importance of fatigue for aircraft structural failures and the sources of fatigue nucleation and cracking, (ii) contemporary FCG lifing methods, and (iii) the Quantitative Fractography (QF) required for determining the actual FCG behaviour. These surveys are followed by the main part of the book, which is a discussion, using case histories, of the applicabilities of Linear Elastic Fracture Mechanics (LEFM) and non-LEFM methods for analysing service fatigue failures and full- and sub-scale test results. This discussion is derived primarily from the experiences of the Defence Science and Technology Group in Melbourne, Australia, and the Netherlands Aerospace Centre, Marknesse, the Netherlands.
1 Historical Review.- 1.1 FCG Parameters, Concepts and Testing.- 1.2 FCG Laws and Models.- 1.3 Summary.- 2 Basic Information for Aircraft FCG Failure and Lifing Analyses.- 2.1 Importance of Fatigue for Aircraft Structural Failures.- 2.2 Fatigue Crack Nucleation, Discontinuities, Early FCG and Damage Tolerance.- 2.3 Summary of FCG Lifing Methods.- 3 Quantitative Fractography (QF) for FCG analyses.- 3.1 Introduction.- 3.2 Fatigue Striation FCG Analyses.- 3.3 Progression Marking FCG Analyses.- 3.4 Fatigue-nucleating Discontinuities and Equivalent Pre-crack Sizes (EPS).- 3.5 QF Techniques for Fatigue Fracture Surfaces.- 3.6 A Cautionary Note.- 4 Aermacchi MB-326H Wing Spar (1990): Exponential FCG Analysis.- 4.1 Introduction.- 4.2 FCG Analysis for the Failed Spar.- 4.3 Further Examination of Wing Spars.- 4.4 Lessons Learned.- 5 P&W 125B Engine Bearing (1994): 2-Stage Exponential FCG Analysis.- 5.1 Introduction.- 5.2 The Failed No.3 Bearing: Macroscopic and |Metallographic Examination.- 5.3 Cage Failure and FCG Analysis.- 5.4 InterpretalÃ,