Fatigue Analysis to Determine the Repair Limit for the Damaged Fastener Hole of Aging Aircraft(P-3CK)
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Kim, Young-Jin
(Sacheon Regional Center, Defense Agency for Technology and Quality)
Kim, Hyeung-Geun (Sacheon Regional Center, Defense Agency for Technology and Quality) Kim, Chang-Young (Sacheon Regional Center, Defense Agency for Technology and Quality) Chang, Joong-Jin (Sacheon Regional Center, Defense Agency for Technology and Quality) Lee, Mal-Young (Sacheon Regional Center, Defense Agency for Technology and Quality) |
1 | Seokbong Song, The report of Quality Assurance Activity on the first aircraft of P-3CKs in Korea, DTaQ-10-2312-Q, DTaQ, 2010, pp. 56-57. |
2 | Michael C.Y.NIU, Airframe Structural Design, Hongkong Conmilit Press LTD, 1998 |
3 | K.N. Shivakumar, J.C. Newman Jr., "Stress Concentrations for Straight-Shank and Countersunk Holes in Plates Subjected to Tension, Bending, and Pin Loading," NASATP-3192, June 1992 |
4 | Crews, John H., C.S. Hong, and I.S. Raju, "Stress Concentration Factors for Finite Orthotropic Laminates with a Pin-Loaded Hole," NASA-TP-1862, 1981 |
5 | Chul-Young Park, Alten F. Grandt Jr., "Effect of load transfer on the cracking behavior at a countersunk fastener hole," International Journal of Fatigue, 29, 2007, pp. 146-157. DOI ScienceOn |
6 | R.H. Oskouei, M. Keikhosravy, C. Soutis, "A finite element stress analysis of aircraft bolted joints loaded in tension," The Aeronautical Journal, Volume 114 No 1156, May 2010, pp. 315-320. DOI |
7 | J.B. de JONGE, "A Standardized Load Sequence for Flight Simulation Test on Transport Aircraft Wing Structures," Nat. Aerospace Lab, NRL, 1973 |
8 | J. Schijve, A.M. Vlutters, Crack Growth in Aluminium Alloy Sheet Material Under Flight-Simulation Loading, Delft University of Technology LR-441, 1984 9 |
9 | Ulf G. Goranson, "Damage Tolerance Facts and Friction," International Conference on Damage Tolerance of Aircraft Structures, 2007 Sep. |
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