PSI - Issue 28
Rhys Jones et al. / Procedia Structural Integrity 28 (2020) 364–369 Rhys Jones/ Structural Integrity Procedia 00 (2019) 000–000
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http://www.tc.faa.gov/its/worldpac/techrpt/tc16-15.pdf (accessed on 04/20/2020). 3. Department of Defense Joint Service Specification Guide, Aircraft Structures, JSSG-2006, October 1998.
4. MIL-STD-1530D, 2016. Department Of Defense Standard Practice: Aircraft Structural Integrity Program (ASIP), 31-Aug-2016. 5. S.B. EZ-SB-19-01, 2019. Durability and Damage Tolerance Certification for Additive Manufacturing of Aircraft Structural Metallic Parts, Wright Patterson Air Force Base, OH, USA, 10 June 2019. Available online: http:// https://daytonaero.com/usaf-structures-bulletins-library/ (accessed on 04/20/2020). 6. Kundu, S., Jones, R., Peng, D., Matthews, N., Alankar A., Raman, SR., Huang, P., 2020. Review of requirements for the durability and damage tolerance certification of additively manufactured aircraft structural parts and AM repairs, Materials, vol. 13, doi:10.3390/ma13061341. 7. Lincoln, JW., Melliere, RA., 1999. Economic life determination for a military aircraft, Journal of aircraft, vol. 36, pp. 737-742. 8. ASTM-E647-15,,2015. Standard test method for measurement of fatigue crack growth rates, Annual Book of ASTM Standards, vol. 03.01. 9. Iliopoulos, A.P.,Jones, R., Michopoulos, JG., Phan, N., and Raman, RS., 2018. Crack growth in a range of additively manufactured aerospace structural materials, Aerospace, 5, 118-136. 10. Iliopoulos, AP., Jones, R., Michopoulos, JG., Phan, N. and Rans, C, 2020. Further Studies into Crack Growth in Additively Manufactured Materials, Materials, 13, 2223; doi:10.3390/ma13102223 11. Jones, R., Michopoulos, JG., Illiopoulos, AP., Raman, RS., Phan, N., and T. Nguyen, 2018. Representing crack growth in additively manufactured Ti-6Al-4V, International Journal of Fatigue, 116, 610-622. 12. Schwalbe, K-H., 2011. On the beauty of analytical models for fatigue crack propagation and fracture-A personal historical review, Fatigue and Fracture Mechanics, 37, 3-73, doi:10.1520/JAI102713. 13. Jones, R., 2014. Fatigue crack growth and damage tolerance, Fatigue & Fracture of Engineering Materials & Structures, 37, 463-483. 14. Jones, R., Raman, RS., and McMillan, A., 2018. Crack growth: Does microstructure play a role? Engineering Fracture Mechanics, 187, 190 210. 15. Fatemi, A., Molaei, R., Phan, N., 2020. Multiaxial fatigue of additive manufactured metals: performance, analysis, and applications, International Journal of Fatigue, 134, doi: https://doi.org/10.1016/j.ijfatigue.2020.105479. 16. Fatemi, A., Molaei, R., Sharifimehr, S., Phan, N., Shamsaei, N., 2017., Multiaxial fatigue behaviour of wrought and additive manufactured Ti-6Al-4V including surface finish effect, International Journal of Fatigue, 100, 347-366. 17. Bergman, M., 1995. Stress intensity factors for circumferential surface cracks in pipes, Fatigue & Fracture of Engineering Materials & Structures, 18, 1155-1172. 18. Liu, A., 1996. Summary of stress-intensity factors, ASM Handbook: Fatigue and Fracture , 19, 980-1000. 19. Edwards, P., Ramulu, M., 2015. Effect of build direction on the fracture toughness and fatigue crack growth in selective laser melted Ti ‐ 6Al ‐ 4V, Fatigue & Fracture of Engineering Materials & Structures, 38, 1228-1236.
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