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Volumn 21, Issue SUPPL. 1, 1999, Pages

A comparison of fatigue crack formation at holes in 2024-T3 and 2524-T3 aluminum alloy specimens

Author keywords

Aluminum alloys; Multiple site damage; Widespread fatigue damage

Indexed keywords

ALUMINUM SHEET; CORROSION; CRACK PROPAGATION; CYCLIC LOADS; FATIGUE OF MATERIALS; FUSELAGES; PERFORMANCE;

EID: 0033228357     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Review
Times cited : (44)

References (11)
  • 3
    • 0031121892 scopus 로고    scopus 로고
    • Effect of prior corrosion on the S/N fatigue performance of aluminum sheet alloys 2024-T3 and 2524-T3
    • Van der Sluys WA, Piascik RS, Zawierucha R, editors Philadelphia: American Society for Testing and Materials
    • Bray GH, Bucci RJ, Colvin EL, Kulak M. Effect of prior corrosion on the S/N fatigue performance of aluminum sheet alloys 2024-T3 and 2524-T3. In: Van der Sluys WA, Piascik RS, Zawierucha R, editors. Effects of environment on the initiation of crack growth, ASTM STP 1298. Philadelphia: American Society for Testing and Materials, 1997.
    • (1997) Effects of Environment on the Initiation of Crack Growth, ASTM STP 1298
    • Bray, G.H.1    Bucci, R.J.2    Colvin, E.L.3    Kulak, M.4
  • 4
    • 0346199666 scopus 로고
    • Standard practice for evaluating intergranular corrosion resistance of heat treatable aluminum alloys by immersion in sodium chloride+hydrogen peroxide solution, ASTM G1 10-92
    • vol. 03.02. American Society for Testing and Materials
    • Standard practice for evaluating intergranular corrosion resistance of heat treatable aluminum alloys by immersion in sodium chloride+hydrogen peroxide solution, ASTM G1 10-92. In: Annual book of ASTM standards, vol. 03.02. American Society for Testing and Materials, 1987:456-7.
    • (1987) Annual Book of ASTM Standards , pp. 456-457
  • 6
    • 11544310717 scopus 로고    scopus 로고
    • Lower wing disassembly and inspection results of two high time USAF B707 aircraft
    • WL-TR-97-4054, June
    • Luzar J, Hug A. Lower wing disassembly and inspection results of two high time USAF B707 aircraft. In: Proceedings of the 1996 USAF Structural Integrity Program Conference, vol. I, WL-TR-97-4054, June 1997:509-28.
    • (1997) Proceedings of the 1996 USAF Structural Integrity Program Conference , vol.1 , pp. 509-528
    • Luzar, J.1    Hug, A.2
  • 7
    • 0003395796 scopus 로고
    • Stress intensity factor equations for cracks in three-dimensional finite bodies
    • Newman JC Jr, Raju IS. Stress intensity factor equations for cracks in three-dimensional finite bodies. NASA Technical Memorandum 83200, 1981:1-49.
    • (1981) NASA Technical Memorandum 83200 , pp. 1-49
    • Newman J.C., Jr.1    Raju, I.S.2
  • 8
    • 0020848601 scopus 로고
    • Stress intensity factors of hole edge cracks. Comparison between one crack and two symmetric cracks
    • Schijve J. Stress intensity factors of hole edge cracks. Comparison between one crack and two symmetric cracks. Int J Fract 1983;23:R111-5.
    • (1983) Int J Fract , vol.23
    • Schijve, J.1
  • 9
    • 0021596018 scopus 로고
    • Transition of part-through cracks at holes into through the thickness flaws
    • Sanford RJ, editor Philadelphia: American Society for Testing and Materials
    • Grandt AF Jr, Harter JA, Heath BJ. Transition of part-through cracks at holes into through the thickness flaws. In: Sanford RJ, editor. Fracture mechanics: fifteenth symposium, ASTM STP 833. Philadelphia: American Society for Testing and Materials, 1984:7-23.
    • (1984) Fracture Mechanics: Fifteenth Symposium, ASTM STP 833 , pp. 7-23
    • Grandt A.F., Jr.1    Harter, J.A.2    Heath, B.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.