메뉴 건너뛰기




Volumn 69, Issue 3-4, 2009, Pages 396-405

Post-stretching induced stress redistribution in Fibre Metal Laminates for increased fatigue crack growth resistance

Author keywords

B. Fatigue; B. Mechanical properties; C. Damage tolerance; C. Residual stress; Fibre metal laminates

Indexed keywords

ARCH BRIDGES; CRACKING (CHEMICAL); CRACKS; DAMAGE TOLERANCE; FATIGUE CRACK PROPAGATION; FATIGUE DAMAGE; FATIGUE OF MATERIALS; FIBERS; FITS AND TOLERANCES; GROWTH (MATERIALS); MECHANICAL PROPERTIES; METALS; PROGRAMMING THEORY; RESIDUAL STRESSES; STRENGTH OF MATERIALS; STRESS CONCENTRATION; STRESS-STRAIN CURVES; STRESSES; THERMAL EXPANSION; THERMAL SPRAYING; UNLOADING;

EID: 59149106355     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compscitech.2008.11.006     Document Type: Article
Times cited : (72)

References (37)
  • 1
    • 59149098155 scopus 로고    scopus 로고
    • Heinimann MB, Bucci RJ, Kulak M, Garratt M. Improving damage tolerance of aircraft structures through the use of selective reinforcement. In: Donne C, editor. Structural integrity of advanced aircraft and life extension for current fleets - lessons learned in 50 years after the comet accidents, vol. 1. EMAS, Sheffield; 2005. p. 197-208.
    • Heinimann MB, Bucci RJ, Kulak M, Garratt M. Improving damage tolerance of aircraft structures through the use of selective reinforcement. In: Donne C, editor. Structural integrity of advanced aircraft and life extension for current fleets - lessons learned in 50 years after the comet accidents, vol. 1. EMAS, Sheffield; 2005. p. 197-208.
  • 2
    • 59149106925 scopus 로고    scopus 로고
    • Honselaar C. The residual internal stress distrubution in arall. Master's thesis, Delft University of Technology, Delft, 1986.
    • Honselaar C. The residual internal stress distrubution in arall. Master's thesis, Delft University of Technology, Delft, 1986.
  • 3
    • 59149085468 scopus 로고    scopus 로고
    • Pegels CS. A study on the residual stress of GLARE 1. Master's thesis, Delft University of Technology, Delft, August 1995.
    • Pegels CS. A study on the residual stress of GLARE 1. Master's thesis, Delft University of Technology, Delft, August 1995.
  • 4
    • 59149102472 scopus 로고    scopus 로고
    • Vogelesang LB, Marissen R, Schijve J. A new fatigue resistant material: aramid aluminum laminate. In: 11th ICAF symposium, 1981.
    • Vogelesang LB, Marissen R, Schijve J. A new fatigue resistant material: aramid aluminum laminate. In: 11th ICAF symposium, 1981.
  • 6
    • 0036535004 scopus 로고    scopus 로고
    • Fatigue damage in titanium-graphite hybrid laminate
    • Buianek D.A., and Spearing S.M. Fatigue damage in titanium-graphite hybrid laminate. Compos Sci Technol 62 (2002) 607-617
    • (2002) Compos Sci Technol , vol.62 , pp. 607-617
    • Buianek, D.A.1    Spearing, S.M.2
  • 7
    • 0029755468 scopus 로고    scopus 로고
    • Fatigue delamination growth in carbon fiber-reinforced aluminium laminate
    • Lin C.T., and Kao P.W. Fatigue delamination growth in carbon fiber-reinforced aluminium laminate. Compos Part A 27A 1 (1996) 9-15
    • (1996) Compos Part A , vol.27 A , Issue.1 , pp. 9-15
    • Lin, C.T.1    Kao, P.W.2
  • 10
    • 0142007778 scopus 로고    scopus 로고
    • An historic overview of the development of fibre metal laminate
    • Vermeeren C.A.J.R. An historic overview of the development of fibre metal laminate. Appl Compos Mater 10 (2003) 189-205
    • (2003) Appl Compos Mater , vol.10 , pp. 189-205
    • Vermeeren, C.A.J.R.1
  • 11
    • 59149106038 scopus 로고    scopus 로고
    • Fredell R. The development of inspection and repair methods for the C-17 aft cargo door. Tech. Rep. LR-704, Faculty of Aerospace Engineering, Delft, November 1992.
    • Fredell R. The development of inspection and repair methods for the C-17 aft cargo door. Tech. Rep. LR-704, Faculty of Aerospace Engineering, Delft, November 1992.
  • 12
    • 59149101058 scopus 로고    scopus 로고
    • Cook J. Processing and properties of high temperature metal/fiber-reinforced-thermoplastic laminates. Tech. Rep. AD-A278 791, Air Vehicle and Crew Systems Technology Department, Warminster, PA, October 1993.
    • Cook J. Processing and properties of high temperature metal/fiber-reinforced-thermoplastic laminates. Tech. Rep. AD-A278 791, Air Vehicle and Crew Systems Technology Department, Warminster, PA, October 1993.
  • 13
    • 0033279213 scopus 로고    scopus 로고
    • Toward application of fibre metal laminates in large aircraft
    • Vlot A., Vogelesang L.B., and Vries T.F. Toward application of fibre metal laminates in large aircraft. Aircraft Eng Aerosp Technol 71 (1999) 558-570
    • (1999) Aircraft Eng Aerosp Technol , vol.71 , pp. 558-570
    • Vlot, A.1    Vogelesang, L.B.2    Vries, T.F.3
  • 14
    • 0003031031 scopus 로고
    • On the application of Glare for airbus fuselage structures
    • Beuker A., de Jong T., Sinke J., and Vogelesang L.B. (Eds), Delft University Press
    • Schwarmann L., Ohrloff N., and Beumler T. On the application of Glare for airbus fuselage structures. In: Beuker A., de Jong T., Sinke J., and Vogelesang L.B. (Eds). Fatigue of aircraft materials (1992), Delft University Press 191-198
    • (1992) Fatigue of aircraft materials , pp. 191-198
    • Schwarmann, L.1    Ohrloff, N.2    Beumler, T.3
  • 15
    • 59149089327 scopus 로고    scopus 로고
    • Khan SU, Alderliesten RC, Benedictus R. Fatigue crack growth in fiber metal laminate under variable amplitude loading. In: International council of aeronautical sciences (ICAS), 2008.
    • Khan SU, Alderliesten RC, Benedictus R. Fatigue crack growth in fiber metal laminate under variable amplitude loading. In: International council of aeronautical sciences (ICAS), 2008.
  • 16
    • 59149104220 scopus 로고    scopus 로고
    • Roebroeks GHJJ. Towards Glare, the development of a fatigue insensitive and damage tolerant aircraft material. PhD thesis, Delft University of Technology, Delft, 1991.
    • Roebroeks GHJJ. Towards Glare, the development of a fatigue insensitive and damage tolerant aircraft material. PhD thesis, Delft University of Technology, Delft, 1991.
  • 17
    • 0040419468 scopus 로고
    • Fibre-metal laminates recent developments and applications
    • Roebroeks G.H.J.J. Fibre-metal laminates recent developments and applications. Int J Fatigue 16 1 (1994) 33-42
    • (1994) Int J Fatigue , vol.16 , Issue.1 , pp. 33-42
    • Roebroeks, G.H.J.J.1
  • 18
    • 59149103265 scopus 로고    scopus 로고
    • Alderliesten RC, Woerden HJM. Load history effects during fatigue crack propagation in Glare. In: Guillaume M, editor. Fatigue of aeronautical structures as an engineering challenge, vol. I; 2003. p. 509-30.
    • Alderliesten RC, Woerden HJM. Load history effects during fatigue crack propagation in Glare. In: Guillaume M, editor. Fatigue of aeronautical structures as an engineering challenge, vol. I; 2003. p. 509-30.
  • 20
    • 59149097703 scopus 로고    scopus 로고
    • Vogelesang LB, Marissen R, Schijve J. Aircraft fatigue in the eighties. In: Proceedings of the 11th ICAF symposium, Noordwijkerhout, Netherlands, 1981. p. 3.4/1.
    • Vogelesang LB, Marissen R, Schijve J. Aircraft fatigue in the eighties. In: Proceedings of the 11th ICAF symposium, Noordwijkerhout, Netherlands, 1981. p. 3.4/1.
  • 21
    • 59149104875 scopus 로고    scopus 로고
    • Vogelesang LB, Gunnink JW. Arall, a material for the next generation of aircraft - a state of the art. Tech. Rep. LR-400, Department of Aerospace Engineering, Delft University of Technology, Netherlands, August 1983.
    • Vogelesang LB, Gunnink JW. Arall, a material for the next generation of aircraft - a state of the art. Tech. Rep. LR-400, Department of Aerospace Engineering, Delft University of Technology, Netherlands, August 1983.
  • 23
    • 30344438821 scopus 로고    scopus 로고
    • Fatigue initiation in fibre metal laminates
    • Homan J.J. Fatigue initiation in fibre metal laminates. Int J Fatigue 28 (2006) 366-374
    • (2006) Int J Fatigue , vol.28 , pp. 366-374
    • Homan, J.J.1
  • 24
    • 59149103884 scopus 로고    scopus 로고
    • Marissen R. Fatigue crack growth in arall, a hybrid aluminium-aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate. PhD thesis, Delft University of Technology, Delft, 1988.
    • Marissen R. Fatigue crack growth in arall, a hybrid aluminium-aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate. PhD thesis, Delft University of Technology, Delft, 1988.
  • 25
    • 59149100603 scopus 로고    scopus 로고
    • Alderliesten RC. Fatigue crack propagation and delamination growth in Glare. PhD thesis, Delft University of Technology, Delft, 2005.
    • Alderliesten RC. Fatigue crack propagation and delamination growth in Glare. PhD thesis, Delft University of Technology, Delft, 2005.
  • 26
    • 33845625682 scopus 로고    scopus 로고
    • Analytical prediction model for fatigue crack propagation and delamination growth in Glare
    • Alderliesten R.C. Analytical prediction model for fatigue crack propagation and delamination growth in Glare. Int J Fatigue 29 (2007) 628-646
    • (2007) Int J Fatigue , vol.29 , pp. 628-646
    • Alderliesten, R.C.1
  • 31
    • 0019398428 scopus 로고
    • Some formulas for the crack opening stress level
    • Schijve J. Some formulas for the crack opening stress level. Eng Fract Mech 14 (1981) 461-465
    • (1981) Eng Fract Mech , vol.14 , pp. 461-465
    • Schijve, J.1
  • 32
    • 59149099706 scopus 로고    scopus 로고
    • Rensma E. Investigation of innovative concepts for hybrid structures. Master's thesis, Delft University of Technology, Delft, 2007.
    • Rensma E. Investigation of innovative concepts for hybrid structures. Master's thesis, Delft University of Technology, Delft, 2007.
  • 33
    • 85086607405 scopus 로고    scopus 로고
    • Khan SU, Alderliesten RC, Benedictus R. LDA's applicability for predicting fatigue crack growth in FMLs under VA loading. In: 49th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Schaumburg, IL, No. AIAA-2008-2017 in AIAA, 2008.
    • Khan SU, Alderliesten RC, Benedictus R. LDA's applicability for predicting fatigue crack growth in FMLs under VA loading. In: 49th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Schaumburg, IL, No. AIAA-2008-2017 in AIAA, 2008.
  • 34
    • 59149102087 scopus 로고    scopus 로고
    • Schijve J, Jacobs FA, Tromp PJ. Fatigue crack growth in aluminium alloy sheet material specimens under flight simulation loading. Effects of design stress level and loading frequency. Tech. Rep. NLR-TR 72019U, NLR-Amsterdam, The Netherlands, 1972.
    • Schijve J, Jacobs FA, Tromp PJ. Fatigue crack growth in aluminium alloy sheet material specimens under flight simulation loading. Effects of design stress level and loading frequency. Tech. Rep. NLR-TR 72019U, NLR-Amsterdam, The Netherlands, 1972.
  • 35
    • 0021619194 scopus 로고
    • A contribution to the evaluation of sequence effects under variable amplitude loading by applying defined predeformations
    • Sih G., Sommer E., and Dahl W. (Eds), Martinus Nijhoff Publisher
    • Schulte K., Marissen R., Trautmann K.-H., and Nowack H. A contribution to the evaluation of sequence effects under variable amplitude loading by applying defined predeformations. In: Sih G., Sommer E., and Dahl W. (Eds). Application of fracture mechanics to materials and structures (1984), Martinus Nijhoff Publisher 777-785
    • (1984) Application of fracture mechanics to materials and structures , pp. 777-785
    • Schulte, K.1    Marissen, R.2    Trautmann, K.-H.3    Nowack, H.4
  • 36
    • 0344196423 scopus 로고
    • The effect of pre-strain on fatigue crack growth and crack closure
    • Schijve J. The effect of pre-strain on fatigue crack growth and crack closure. Eng Fract Mech 8 (1976) 575-581
    • (1976) Eng Fract Mech , vol.8 , pp. 575-581
    • Schijve, J.1
  • 37
    • 0016317295 scopus 로고
    • The effect of pre-stress cycles on fatigue crack growth - an analysis of the crack growth mechanism
    • Kang T., and Liu H. The effect of pre-stress cycles on fatigue crack growth - an analysis of the crack growth mechanism. Eng Fract Mech 6 (1974) 631-638
    • (1974) Eng Fract Mech , vol.6 , pp. 631-638
    • Kang, T.1    Liu, H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.