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Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components

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Cover of 'Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components'

Table of Contents

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    Book Overview
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    Chapter 1 Historical Review
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    Chapter 2 Basic Information for Aircraft FCG Failure and Lifing Analyses
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    Chapter 3 Quantitative Fractography (QF) for FCG Analyses
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    Chapter 4 Aermacchi MB-326H Wing Spar (1990): Exponential FCG Analysis
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    Chapter 5 P&W 125B Engine Bearing (1994): 2-Stage Exponential FCG Analysis
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    Chapter 6 EBA Example Lifing Assessment (2004): F/A-18 Horizontal Stabilator Spindles
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    Chapter 7 LCFLF Example Lifing Assessment (2004): F/A-18 Vertical Tail Attachment Stubs
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    Chapter 8 Cubic Rule Life Prediction Examples
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    Chapter 9 Fokker 100 Fuselage Test: Lap Joints Exponential FCG Analysis
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    Chapter 10 Sikorsky S-61N Rotor Blade (1974): Exponential FCGR Analysis
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    Chapter 11 Westland Lynx Rotor Hub (1998): Progression Marking LEFM Analysis
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    Chapter 12 Closing Remarks
Attention for Chapter 3: Quantitative Fractography (QF) for FCG Analyses
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