1 |
B. L. Smith, A. Hijazi, A. K. M. Haque, and R. Y. Myose, "Strength of Stiffened 2024-T3 Aluminum Panels with Multiple Site Damage," Journal of Aircraft, Vol. 38, No. 4, 2001, pp. 764-768.
DOI
ScienceOn
|
2 |
R. Galatolo, and K. F. Nilsson, "An Experimental and Numerical Analysis of Residual Strength of Butt-Joints Panels with Multiple Site Damage," Engineering Fracture Mechanics, Vol. 68, No. 13, 2001, pp. 1437-1461.
DOI
ScienceOn
|
3 |
황정선, 조환기, 김주언, "Al 5052-H18의 피로균열 성장지연 연구", 2002년도 종합학술대회논문집, Vol. II, 2002, pp. 839-842.
|
4 |
황정선, 조환기, "예비압입에 의한 알루미늄 2024-T3 알클래드 합금의 균열성장 지연거동", 한국군사과학기술학회지, 제4권, 제2호, 2001, pp. 42-51.
과학기술학회마을
|
5 |
Sam-Hong Song, and Jin-Ho Choi, "Fatigue Crack Retardation by Indentation," Proceedings of Asian Pacific Conference for Fracture and Strength '96, 1996, pp. 57-61.
|
6 |
M. Goto, H. Nisitani, H. Miyagawa, A. Miura, and K. Imado, "Effect of indentation on the Fatigue Strength of Plate Specimens with a Central Notch," 일본기계학회논문집(A편), Vol. 57, No. 544, 1991, pp. 2873-2878.
|
7 |
M. Goto, H. Nisitani, H. Miyagawa, and K. Imado, "Effect of Indentation on the Fatigue Strength of Plate Specimens with a Crack," 일본기계학회논문집(A편), Vol. 56, No. 526, 1990, pp. 1348-1353.
|
8 |
H. Miyagawa, and H. Nisitani, "Retardation of Fatigue Crack Propagation due to Additional Holes or indentations in Plate Specimens," Bulletin of JSME, Vol. 28, 1985, pp. 2219-2223.
DOI
ScienceOn
|
9 |
D. B. Marshall, "Geometrical Effects in Elastic/Plastic Indentation," Journal of American Ceramic Society, Vol. 67, 1984, pp. 57-60.
DOI
ScienceOn
|
10 |
E647-95, "Standard Method for Measurement of Fatigue Crack Growth Rates," American Society of Testing and Materials, 1995, Philadelphia.
|
11 |
T. Swift, "Widespread Fatigue Damage Monitoring-Issues and Concerns," Proceedings of the 5th International Conference on Structural Airworthiness of New and Aging Aircraft, Washington DC, 1993, pp. 133-150.
|
12 |
J. R. Maclin, "Performance of Fuselage Pressure Structure," International Conference on Aging Aircraft and Structural Airworthiness, NASA CP 3160, 1991, pp. 67-74.
|
13 |
B. Smith, A. Mouak, P. Saville, R. Myose, and W. Horn, "Improved Engineering Methods for Determining the Critical Strengths of Aluminium Panels with Multiple Site Damages in Aging Aircraft," NASA Conference Publications, Vol. 208982, No. 2, 1999, pp. 525-534.
|