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Volumn , Issue , 2006, Pages 507-522

Advances in smart-patch repair of aircraft panels

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PANELS; DISBOND; PIEZOELECTRIC PATCH;

EID: 84867865842     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (11)
  • 2
    • 0023418404 scopus 로고
    • Fibre composite repair of cracked metallic aircraft components - Practical and basic aspects
    • DOI 10.1016/0010-4361(87)90293-X
    • Baker, A. A. 1987. "Fiber Composite Repair of Cracked Metallic Aircraft Components -Practical and Basic Aspects," Composites, 18 (4): 293-308. (Pubitemid 18519151)
    • (1987) Composites , vol.18 , Issue.4 , pp. 293-308
    • Baker, A.A.1
  • 3
    • 0032676829 scopus 로고    scopus 로고
    • Repair Substantiation for a bonded composite repair to FIII lower wing skin
    • Baker, A. A., L R. F. Rose, K F. Walker, and E. S. Wilson. 1999. "Repair Substantiation for a Bonded Composite Repair to FIII Lower Wing Skin," Appl. Compos. Mater., 6 (4): 251-267
    • (1999) Appl. Compos. Mater. , vol.6 , Issue.4 , pp. 251-267
    • Baker, A.A.1    Rose, R.F.L.2    Walker, F.K.3    Wilson, E.S.4
  • 4
    • 0033304354 scopus 로고    scopus 로고
    • Bonded composite repair of fatigue-cracked primary aircraft structure
    • Baker, A. 1999. "Bonded Composite Repair of Fatigue-Cracked Primary Aircraft Structure," Compos. Struct., 47 (1-4): 431-443.
    • (1999) Compos. Struct , vol.47 , Issue.1-4 , pp. 431-443
    • Baker, A.1
  • 5
    • 0034352964 scopus 로고    scopus 로고
    • Smart structure application in bonded repairs
    • Chiu, W. K., Y L Koh, S. C Galea, and N. Rajic. 2000. "Smart Structure Application in Bonded Repairs," Compos. Struct., 50 (4): 433-444.
    • (2000) Compos. Struct , vol.50 , Issue.4 , pp. 433-444
    • Chiu, W.K.1    Koh, L.Y.2    Galea S, C.3    Rajic, N.4
  • 6
    • 0034541655 scopus 로고    scopus 로고
    • Optical fibre sensors for health monitoring of bonded repair systems
    • DOI 10.1016/S0263-8223(00)00107-0
    • McKenzie, I., R. Jones, I. H. Marshall, and S. Galea. 2000. "Optical Fibre Sensors for Health Monitoring of Bonded Repair Systems," Compos. Struct., 50(4): 405-416. (Pubitemid 32022535)
    • (2000) Composite Structures , vol.50 , Issue.4 , pp. 405-416
    • McKenzie, I.1    Jones, R.2    Marshall, I.H.3    Galea, S.4
  • 7
    • 0036853163 scopus 로고    scopus 로고
    • Health monitoring of composite repairs and joints using optical fibres
    • DOI 10.1016/S0263-8223(02)00235-0, PII S0263822302002350
    • Jones, R., and S. Galea. 2002. "Health Monitoring of Composite Repairs and Joints Using Optical Fibres," Compos. Struct., 58 (3): 397-403 (Pubitemid 35374886)
    • (2002) Composite Structures , vol.58 , Issue.3 , pp. 397-403
    • Jones, R.1    Galea, S.2
  • 8
    • 4143123192 scopus 로고    scopus 로고
    • Development of life extension strategies for Australian military aircraft, using structural health monitoring of composite repairs and joints
    • DOI 10.1016/j.compstruct.2004.04.031, PII S0263822304001230
    • Baker, W., I. McKenzie, and R. Jones. 2004. "Development of Life Extension Strategies for Australian Military Aircraft, Using Structural Health Monitoring of Composite Repairs and Joints," Compos. Struct., 66 (1-4): 133-143. (Pubitemid 39102957)
    • (2004) Composite Structures , vol.66 , Issue.1-4 , pp. 133-143
    • Baker, W.1    McKenzie, I.2    Jones, R.3
  • 9
    • 0032660852 scopus 로고    scopus 로고
    • Investigation of a cracked thick aluminum panel repaired with a bonded composite patch
    • Schubbe, J J, and S Mall 1999 "Investigation of a Cracked Thick Aluminum Panel Repaired with a Bonded Composite Patch," Eng. Fraci. Meek, 63 (3): 305-323.
    • (1999) Eng. Fraci. Meek , vol.63 , Issue.3 , pp. 305-323
    • Schubbe, J.J.1    Mall, S.2
  • 10
    • 33745471900 scopus 로고    scopus 로고
    • Identification of location and shape of fatigue crack fronts in aircraft structural panels repaired with a bonded FRP composite patch containing a strain measurement plane
    • Fujimoto, S., and H. Sekine. 2004. "Identification of Location and Shape of Fatigue Crack Fronts in Aircraft Structural Panels Repaired with a Bonded FRP Composite Patch Containing a Strain Measurement Plane,' 'J. Jpn. Soc. Aeronaut. Space Sci., 52 (607): 361-370.
    • (2004) J. Jpn. Soc. Aeronaut. Space Sci. , vol.52 , Issue.607 , pp. 361-370
    • Fujimoto, S.1    Sekine, H.2
  • 11
    • 0002935896 scopus 로고
    • The tunneling algorithm for the global minimization of functions
    • Levy, A. V, and A. Montalvo. 1985. "The Tunneling Algorithm for the Global Minimization of Functions," SUM J. Sci. Struct. Comput., 6(1): 15-29.
    • (1985) SUM J. Sci. Struct. Comput , vol.6 , Issue.1 , pp. 15-29
    • Levy A, V.1    Montalvo, A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.