Author | Wanhill, Russell. author. Author. http://id.loc.gov/vocabulary/relators/aut |
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Title | Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components [electronic resource] / by Russell Wanhill, Simon Barter, Loris Molent |
Imprint | Dordrecht : Springer Netherlands : Imprint: Springer, 2019 |
Edition | 1st ed. 2019 |
Connect to | https://doi.org/10.1007/978-94-024-1675-6 |
Descript | XI, 99 p. 50 illus., 47 illus. in color. online resource |
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 etallographic Examination -- 5.3 Cage Failure and FCG Analysis -- 5.4 Interpretation of the Results, Conclusions, and Remedial Action -- 6. EBA Example Lifing Assessment (2004): F/A-18 Horizontal StabilatorSpindles -- 6.1 Introduction -- 6.2 EBA Validation for the F/A-18 Horizontal Stabilator Spindles -- 6.3 EBA and Total Life Assessment for the F/A-18 Horizontal Stabilator Spindles -- 7. LCFLF Example Lifing Assessment (2004): F/A-18 Vertical Tail Attachment Stubs -- 7.1 Introduction -- 7.2 The FT46 Stub Flange Crack -- 7.3 Fractography of the FT46 Stub Flange Crack -- 7.4 LCFLF Life Assessment for the FT46 Stub Flange Crack -- 8. Cubic Rule Life Prediction Examples -- 8.1 Introduction -- 8.2 McDonnell Douglas F4E Spectrum Coupon Test Data -- 8.3 Lockheed Martin P3C Spectrum Coupon Test Data -- 8.4 Summary -- 9. Fokker 100 Fuselage Test: Lap Joints Exponential FCG Analysis -- 9.1 Introduction -- 9.2 FCG Analysis of the Cracked Lap Splice [71.72.95] -- 10. Sikorsky S-61N Rotor Blade (1974): Exponential FCGR Analysis -- 10.1 Introduction -- 10.2 FCG Analysis for the Crashed Helicopter -- 10.3 Prediction of Detectable FCG Lives -- 10.4 Results and Remedial Actions (Lessons Learned) -- 11. Westland Lynx Rotor Hub (1998): Progression Marking LEFM Analysis -- 11.1 Introduction -- 11.2 Fractography of Early Fatigue Cracking in the M326 Yellow Arm -- 11.3 Fractography of Early Fatigue Cracking in the M6 Arm and M326Specimens -- 11.4 FRTB + LEFM Estimations of Damaging Service Fatigue Stress Levels -- 11.5 Measurements of Service Loads and Fatigue Analysis by GKNW -- 11.6 Causes of Failure and Remedial Action -- 12. Closing Remarks -- References