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Volumn 22, Issue 4, 2000, Pages 319-338

Multiple-site damage in riveted lap-joints: experimental simulation and finite element prediction

Author keywords

[No Author keywords available]

Indexed keywords

AGING OF MATERIALS; ALUMINUM ALLOYS; COMPUTER SIMULATION; CRACK INITIATION; DILATOMETERS; FINITE ELEMENT METHOD; JOINTS (STRUCTURAL COMPONENTS); MATHEMATICAL MODELS;

EID: 0342626770     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(99)00129-2     Document Type: Article
Times cited : (95)

References (30)
  • 1
    • 0343455852 scopus 로고    scopus 로고
    • Structural maintenance of ageing aircraft. BRITE-EURAM project number BE95-1053
    • March
    • Structural maintenance of ageing aircraft. BRITE-EURAM project number BE95-1053, Synthesis report, March 1999.
    • (1999) Synthesis Report
  • 3
    • 0012971719 scopus 로고
    • Fatigue of aircraft materials and structures
    • Schijve J. Fatigue of aircraft materials and structures. Int J Fatigue. 16(1):1994;21-32.
    • (1994) Int J Fatigue , vol.16 , Issue.1 , pp. 21-32
    • Schijve, J.1
  • 4
    • 0041908687 scopus 로고
    • Crack growth from loaded countersunk rivet holes: Durability of metal aircraft structures
    • In: Atluri SN, Harris CE, Hoggard A, Miller N, Sampath SG, editors. 31 March-2 April; Atlanta: Springer Verlag
    • Dawicke DS, Phillips EP, Swenson DV, Gondhalekar S. Crack growth from loaded countersunk rivet holes: durability of metal aircraft structures. In: Atluri SN, Harris CE, Hoggard A, Miller N, Sampath SG, editors. Proceedings of the International Workshop on Structural Integrity of Aging Airplanes, 31 March-2 April; Atlanta: Springer Verlag, 1992. p. 75-90.
    • (1992) Proceedings of the International Workshop on Structural Integrity of Aging Airplanes , pp. 75-90
    • Dawicke, D.S.1    Phillips, E.P.2    Swenson, D.V.3    Gondhalekar, S.4
  • 8
    • 79961052454 scopus 로고
    • The effect of secondary bending on the fatigue strength of joints
    • RAE library translation no. 1858, August
    • Schutz D, Lowak H. The effect of secondary bending on the fatigue strength of joints. Laboratorium fur Betriebsfestigkeit Report FB-113 (1974), RAE library translation no. 1858, August 1975.
    • (1974) Laboratorium fur Betriebsfestigkeit Report , vol.FB-113
    • Schutz, D.1    Lowak, H.2
  • 10
    • 85031607967 scopus 로고
    • The effect of cladding condition on the stages of fatigue crack formation and growth: Problems with fatigue in aircraft
    • Emmen: Swiss Federal Aircraft Establishment (F+W). pp. 2.5/1-2.5/23
    • Forsyth P.J.E. The effect of cladding condition on the stages of fatigue crack formation and growth: problems with fatigue in aircraft. Proceedings of the Eighth ICAF Symposium. 1975;Swiss Federal Aircraft Establishment (F+W), Emmen. pp. 2.5/1-2.5/23.
    • (1975) Proceedings of the Eighth ICAF Symposium
    • Forsyth, P.J.E.1
  • 13
    • 85031600315 scopus 로고
    • Fracture mechanics analysis of short cracks at loaded holes: Behaviour of short cracks in airframe components
    • Neuilly-sur-Seine: Advisory Group for Aerospace Research and Development. pp. 8-1-8-6
    • Rooke D.P. Fracture mechanics analysis of short cracks at loaded holes: behaviour of short cracks in airframe components. AGARD Conference Proceedings No. 328. 1983;Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine. pp. 8-1-8-6.
    • (1983) AGARD Conference Proceedings No. 328
    • Rooke, D.P.1
  • 16
    • 0031335576 scopus 로고    scopus 로고
    • Multiple-site and widespread fatigue damage in aging aircraft
    • Pitt S., Jones R. Multiple-site and widespread fatigue damage in aging aircraft. Eng Failure Anal. 4(4):1997;237-257.
    • (1997) Eng Failure Anal , vol.4 , Issue.4 , pp. 237-257
    • Pitt, S.1    Jones, R.2
  • 17
    • 84970474937 scopus 로고
    • Part 2 of the U.S. National Transportation Safety Board Report on the Fuselage Failure of an Aloha Airlines Boeing 737-200 in April 1988. 4 September-15 September
    • Part 2 of the U.S. National Transportation Safety Board Report on the Fuselage Failure of an Aloha Airlines Boeing 737-200 in April 1988. In: Aviation Week and Space Technology, 4 September-15 September 1989.
    • (1989) In: Aviation Week and Space Technology
  • 21
    • 0027556887 scopus 로고
    • Crack growth and repair of multi-site damage of fuselage lap joints
    • Molent L., Jones R. Crack growth and repair of multi-site damage of fuselage lap joints. Eng Fract Mech. 44(4):1993;627-637.
    • (1993) Eng Fract Mech , vol.44 , Issue.4 , pp. 627-637
    • Molent, L.1    Jones, R.2
  • 22
    • 0003666084 scopus 로고
    • The effects of multi-site damage on the arrest capability of aircraft fuselage structures
    • Broek D. The effects of multi-site damage on the arrest capability of aircraft fuselage structures. FractuREsearch, TR 9302, 1993.
    • (1993) FractuREsearch, TR 9302
    • Broek, D.1
  • 25
    • 85031599403 scopus 로고    scopus 로고
    • Document SMAAC-TR-3.1-01-1.3/NLR, NLR-TR-98195, March
    • van der Hoeven W, Schra L. Document SMAAC-TR-3.1-01-1.3/NLR, NLR-TR-98195, March 1998.
    • (1998)
    • Van Der Hoeven, W.1    Schra, L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.