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Volumn 41, Issue 3-4, 1998, Pages 303-313

Nonlinear analysis of bonded composite patch repair of cracked aluminum panels

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVE JOINTS; ALUMINUM; COMPOSITE STRUCTURES; CRACKS; GEOMETRY; MATHEMATICAL MODELS; NONLINEAR EQUATIONS; STRESS INTENSITY FACTORS;

EID: 0032019598     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(98)00052-X     Document Type: Article
Times cited : (47)

References (21)
  • 2
    • 0040729578 scopus 로고
    • Bonded repair of damage
    • [2] Jones R. Bonded repair of damage. J Aero Soc (India) 1984;36:193-201.
    • (1984) J Aero Soc (India) , vol.36 , pp. 193-201
    • Jones, R.1
  • 3
    • 0019392130 scopus 로고
    • An application of the inclusion analogy for bonded reinforcements
    • [3] Rose LRF. An application of the inclusion analogy for bonded reinforcements. Int J Solids Structures 1981;17:827-838.
    • (1981) Int J Solids Structures , vol.17 , pp. 827-838
    • Rose, L.R.F.1
  • 5
    • 0030079820 scopus 로고    scopus 로고
    • Analysis of cracked aluminum plates repaired with bonded composite patches
    • [5] Sun CT, Klug J, Arendt C. Analysis of cracked aluminum plates repaired with bonded composite patches. AIAA J 1996;34:(2):369-374.
    • (1996) AIAA J , vol.34 , Issue.2 , pp. 369-374
    • Sun, C.T.1    Klug, J.2    Arendt, C.3
  • 6
    • 0027097448 scopus 로고
    • Analysis of patched and stiffened cracked panels using the boundary element method
    • [6] Young MJ, Rooke DP, Cartwright DJ. Analysis of patched and stiffened cracked panels using the boundary element method. Int J Solids Structures 1992;29:(17):2201-2216.
    • (1992) Int J Solids Structures , vol.29 , Issue.17 , pp. 2201-2216
    • Young, M.J.1    Rooke, D.P.2    Cartwright, D.J.3
  • 7
    • 0017913959 scopus 로고
    • A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures
    • [7] Ratwani MM. A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures. J Eng Mater Technol 1978;100:46-51.
    • (1978) J Eng Mater Technol , vol.100 , pp. 46-51
    • Ratwani, M.M.1
  • 8
    • 0018517116 scopus 로고
    • Analysis of cracked adhesively bonded laminated structures
    • [8] Ratwani MM. Analysis of cracked adhesively bonded laminated structures. AIAA J 1979;17:988-994.
    • (1979) AIAA J , vol.17 , pp. 988-994
    • Ratwani, M.M.1
  • 9
    • 0013314907 scopus 로고
    • Characterization of fatigue crack growth in bonded structures - Analysis of cracked bonded structures
    • Air Force Flight Dynamics Laboratory, OH, July
    • [9] Ratwani MM. Characterization of fatigue crack growth in bonded structures - analysis of cracked bonded structures. AFFADL-TR-31, vol. II. Air Force Flight Dynamics Laboratory, OH, July 1977.
    • (1977) AFFADL-TR-31 , vol.2
    • Ratwani, M.M.1
  • 10
    • 0013314907 scopus 로고
    • Characterization of fatigue crack growth in bonded structures - Crack growth prediction in bonded structures
    • Air Force Flight Dynamics Laboratory, OH, July
    • [10] Ratwani MM. Characterization of fatigue crack growth in bonded structures - crack growth prediction in bonded structures. AFFADL-TR-31, vol. I. Air Force Flight Dynamics Laboratory, OH, July 1977.
    • (1977) AFFADL-TR-31 , vol.1
    • Ratwani, M.M.1
  • 11
    • 0030197458 scopus 로고    scopus 로고
    • Modeling of cracked metallic structure with bonded composite patch using three layer technique
    • [11] Naboulsi S, Mall S. Modeling of cracked metallic structure with bonded composite patch using three layer technique. Composite Structures 1996;35:295-308.
    • (1996) Composite Structures , vol.35 , pp. 295-308
    • Naboulsi, S.1    Mall, S.2
  • 12
    • 0030834515 scopus 로고    scopus 로고
    • Thermal effects on adhesively bonded composite patch repair of cracked aluminum panels
    • [12] Naboulsi S, Mall S. Thermal effects on adhesively bonded composite patch repair of cracked aluminum panels. Theor. Appl. Fract. Mech. 1996;26:1-12.
    • (1996) Theor. Appl. Fract. Mech. , vol.26 , pp. 1-12
    • Naboulsi, S.1    Mall, S.2
  • 13
    • 0031084182 scopus 로고    scopus 로고
    • Characterization of fatigue crack growth in aluminum panels with bonded composite patch
    • [13] Naboulsi S, Mall S. Characterization of fatigue crack growth in aluminum panels with bonded composite patch. Composite Structures 1997;37:321-334.
    • (1997) Composite Structures , vol.37 , pp. 321-334
    • Naboulsi, S.1    Mall, S.2
  • 14
    • 0031247090 scopus 로고    scopus 로고
    • Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches
    • [14] Naboulsi S, Mall S. Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches. Theor Appl Fract Mech 1997;28:13-28.
    • (1997) Theor Appl Fract Mech , vol.28 , pp. 13-28
    • Naboulsi, S.1    Mall, S.2
  • 15
    • 0017561766 scopus 로고
    • A finite element calculation of stress intensity factors by a modified crack closure integral
    • [15] Rybicki EF, Kanninen EF. A finite element calculation of stress intensity factors by a modified crack closure integral. Eng Fract Mech 1977;9:931-938.
    • (1977) Eng Fract Mech , vol.9 , pp. 931-938
    • Rybicki, E.F.1    Kanninen, E.F.2
  • 16
    • 0032108260 scopus 로고    scopus 로고
    • Large deflection effects of cracked aluminum plates repaired with bonded composite patches
    • in press
    • [16] Klug J, Sun CT. Large deflection effects of cracked aluminum plates repaired with bonded composite patches. Composite Structures, in press.
    • Composite Structures
    • Klug, J.1    Sun, C.T.2
  • 17
    • 0040729577 scopus 로고
    • Hibbitt, Karlsson and Sorensen, Inc. Pawtucket, RI 02860, USA
    • [17] ABAQUS Finite Element Programs, ABAQUS/Standard 5.6. Hibbitt, Karlsson and Sorensen, Inc. Pawtucket, RI 02860, USA, 1994.
    • (1994) ABAQUS Finite Element Programs, ABAQUS/standard 5.6
  • 18
    • 0040729580 scopus 로고    scopus 로고
    • personal communication. Wright Laboratory, OH
    • [18] Mazza J, personal communication. Wright Laboratory, OH.
    • Mazza, J.1
  • 19
    • 0040729576 scopus 로고    scopus 로고
    • Crack growth in imperfectly bonded composite patch repairs of cracked aluminium panels
    • ICAF 97, Fatigue in New and Ageing Aircraft, 18-20 June Edinburgh, UK.
    • [19] Naboulsi S, Mall S, Denney JJ. Crack growth in imperfectly bonded composite patch repairs of cracked aluminium panels. In ICAF 97, Fatigue in New and Ageing Aircraft, Proceedings of the 19th Symposium of the International Committee on Aeronautical Fatigue, 18-20 June 1997, Edinburgh, UK. Vol. 1, pp. 639-655.
    • (1997) Proceedings of the 19th Symposium of the International Committee on Aeronautical Fatigue , vol.1 , pp. 639-655
    • Naboulsi, S.1    Mall, S.2    Denney, J.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.