Insertion of high-R cycles into random load spectra as fractographic markers
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OpenAlex topics: Probabilistic and Robust Engineering Design
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References (32)
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1. Barter S A, Molent L, Wanhill R J H. Marker Loads for Quantitative Fractography of Fatigue Cracks in Aerospace Alloys [C].Proceedings of the ICAF 2009, Bridging the Gap between Theory and Operational Practice, Dordrecht, Springer Netherlands, 2009: 15-54.10.1007/978-90-481-2746-7_2 ↗
2. Typical fatigue-initiating discontinuities in metallic aircraft structures10.1016/j.ijfatigue.2011.10.017 ↗
3. Material-based failure analysis of a helicopter rotor hub10.1007/BF02717426 ↗
4. Quantitative fractography of fatigue and an illustrative case study10.1016/j.engfailanal.2018.10.013 ↗
5. Barter S, Athiniotis N, Clark G. The identification of fatigue-critical regions during fatigue testing of Macchi MB326H centre section lower booms [C].Proceedings of the, 2012.
6. Service fatigue cracking in an aircraft bulkhead exposed to a corrosive environment10.1016/j.engfailanal.2013.07.036 ↗
7. Fatigue crack growth from flaws in combat aircraft10.1016/j.ijfatigue.2009.09.002 ↗
8. A comparison of crack growth behaviour in several full-scale airframe fatigue tests10.1016/j.ijfatigue.2006.09.015 ↗
9. Molen · Characterisation of equivalent initial flaw sizes in 7050 aluminium alloy · 2006 · 29 · 916
10. Wanhill R J H, Hattenberg T. Fractography-based estimation of fatigue crack “initiation” and growth lives in aircraft components [C].Proceedings of the, 2006.
11. Wanhill R, Barter S, Molent L. Quantitative Fractography (QF) for FCG Analyses WANHILL R, BARTER S, MOLENT L. Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components. Springer Netherlands. 2019: 29-41.10.1007/978-94-024-1675-6_3 ↗
12. An experimental evaluation of fatigue crack growth10.1016/j.engfailanal.2004.04.002 ↗
13. The lead crack fatigue lifing framework10.1016/j.ijfatigue.2010.09.009 ↗
14. Development and application of marker loads for a fatigue crack growth study on a full-scale test article [M]10.2514/6.1976-1513 ↗
15. Mcdonald M, Boykett R P, Jones M. Quantitative fractography markers for determining fatigue crack growth rates in aluminium and titanium aircraft structures [C].Proceedings of the, 2012.
16. Marker load-aided bidirectional fatigue crack growth rate measurement via a semi-elliptical surface crack10.1016/j.ijfatigue.2018.02.010 ↗
17. Fatigue crack growth of a corner crack at the edge of a hole10.1016/j.ijfatigue.2020.105699 ↗
18. Characterization of fatigue crack growth in directed energy deposited Ti-6Al-4V by marker load method10.1016/j.engfracmech.2024.110500 ↗
19. The EIFS-based fatigue life prediction approach of nickel-based single crystals with film cooling holes at elevated temperature10.1016/j.ijfatigue.2022.107272 ↗
20. Fatigue life prediction based on equivalent initial flaw size for Al-Li alloy 2297 under spectrum loading10.1016/j.ijfatigue.2017.04.015 ↗
21. Molent L. A review of equivalent pre-crack sizes in aluminium alloy 7050-T7451. 2014; 37(10): 1055-74. https://doi.org/10.1111/ffe.12214.10.1111/ffe.12214 ↗
22. Equivalent initial damage sizes (EIDS) for type 1C anodised aluminium alloy 7085-T7452 under variable amplitude loading10.1016/j.engfailanal.2023.107578 ↗
23. Manning S D, Yang J N. USAF (U. S. Air Force) Durability Design Handbook: Guidelines for the Analysis and Design of Durable Aircraft Structures [C].Proceedings of the, 1989.
24. NASGRO Reference Manual (version 4.02, September 2002), Fracture mechanics and fatigue crack growth analysis software. NASA Johnson Space Center and Southwest Research Institute, 2002.
25. Influence of crack configurations on fatigue crack growth behavior of Al 2024 alloy10.1016/j.matpr.2023.05.500 ↗
26. On the use of NASGRO software to estimate fatigue crack growth under variable amplitude loading in aluminium alloy 2024-T35110.1016/j.proeng.2015.02.037 ↗
27. Estimations of fatigue life and variability under random loading in aluminum Al-2024T351 using strip yield models from NASGRO10.1016/j.ijfatigue.2015.09.031 ↗
28. In-situ experimental study on the fatigue crack propagation behavior of 7075-T6 and 2024-T3 aluminium alloys under variable amplitude loading and retardation model modification10.1016/j.tafmec.2022.103372 ↗
29. Newman. Stress-intensity factor equations for cracks in three-dimensional finite bodies. 1981.
30. Probabilistic durability analysis methods for metallic airframes10.1016/0266-8920(87)90026-9 ↗
31. A simple second order approximation for stochastic crack growth analysis10.1016/0013-7944(95)00130-1 ↗
32. Use of standardized sequences of flight-by-flight load spectra in fatigue testing of structural aircraft components10.1016/0013-7944(77)90025-X ↗