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Volumn 35, Issue 6, 2000, Pages 493-505

Investigation of shape optimization for the design of life extension options for an F/A-18 airframe FS 470 bulkhead

Author keywords

[No Author keywords available]

Indexed keywords

ADHESION; CRACK PROPAGATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; OPTIMIZATION; REINFORCEMENT; SENSITIVITY ANALYSIS; STRESS ANALYSIS; STRESS CONCENTRATION; VECTORS;

EID: 0034313650     PISSN: 03093247     EISSN: None     Source Type: Journal    
DOI: 10.1243/0309324001514251     Document Type: Article
Times cited : (29)

References (16)
  • 2
    • 0000528263 scopus 로고
    • A new method of structural shape optimisation based on biological growth
    • Mattheck, C. and Burkhardt, S. A new method of structural shape optimisation based on biological growth. Int. J. Fatigue, 1990, 12(3), 185-190.
    • (1990) Int. J. Fatigue , vol.12 , Issue.3 , pp. 185-190
    • Mattheck, C.1    Burkhardt, S.2
  • 3
    • 0018324927 scopus 로고
    • An optimisation procedure for stress concentrations by the finite element technique
    • Schnack, E. An optimisation procedure for stress concentrations by the finite element technique. Int. J. Numer. Meth. Engng, 1979, 14, 115-124.
    • (1979) Int. J. Numer. Meth. Engng , vol.14 , pp. 115-124
    • Schnack, E.1
  • 5
    • 0033308846 scopus 로고    scopus 로고
    • A gradientless finite element procedure for shape optimization
    • Heller, M., Kaye, R. and Rose, L. R. F. A gradientless finite element procedure for shape optimization. J. Strain Analysis, 1999, 34(5), 323-336.
    • (1999) J. Strain Analysis , vol.34 , Issue.5 , pp. 323-336
    • Heller, M.1    Kaye, R.2    Rose, L.R.F.3
  • 7
    • 0343539380 scopus 로고    scopus 로고
    • Life extension of F/A-18 inboard aileron hinges by shape optimisation and composite reinforcement
    • (Ed. R. Chester), Report DSTO-TR-0699, Ch. 3 (Defence Science and Technology Organisation, Australian Department of Defence, Melbourne)
    • Heller, M., Kaye, R., Whitehead, S. and Lubac, J. Life extension of F/A-18 inboard aileron hinges by shape optimisation and composite reinforcement. In Design and Stress Analysis (Ed. R. Chester), Report DSTO-TR-0699, 1999, Ch. 3 (Defence Science and Technology Organisation, Australian Department of Defence, Melbourne).
    • (1999) Design and Stress Analysis
    • Heller, M.1    Kaye, R.2    Whitehead, S.3    Lubac, J.4
  • 9
    • 0004170839 scopus 로고
    • NASA CR-112235, National Aeronautics and Space Administration
    • Hart-Smith, L. J. Adhesive double lap joints. NASA CR-112235, National Aeronautics and Space Administration, 1973.
    • (1973) Adhesive Double Lap Joints
    • Hart-Smith, L.J.1
  • 10
    • 0003073696 scopus 로고
    • Theoretical analysis of crack patching
    • (Eds A. A. Baker and R. Jones), Ch. 5 (Martinus Nijhoff, The Hague)
    • Rose, L. F. R. Theoretical analysis of crack patching. In Bonded Repair of Aircraft Structures (Eds A. A. Baker and R. Jones), 1988, Ch. 5 (Martinus Nijhoff, The Hague).
    • (1988) Bonded Repair of Aircraft Structures
    • Rose, L.F.R.1
  • 12
    • 0022146152 scopus 로고
    • Optimisation of bonded joints
    • January
    • Ojalvo, I. U. Optimisation of bonded joints. Am. Inst. Aeronaut. Astronaut. J., January 1985, 23 (10), 1578-1582.
    • (1985) Am. Inst. Aeronaut. Astronaut. J. , vol.23 , Issue.10 , pp. 1578-1582
    • Ojalvo, I.U.1
  • 13
    • 0026241253 scopus 로고
    • Shape optimisation of bonded joints
    • Groth, H. L. and Norlund, P. Shape optimisation of bonded joints. Int. J. Adhesion Adhes., 1991, 11(4), 204-212.
    • (1991) Int. J. Adhesion Adhes. , vol.11 , Issue.4 , pp. 204-212
    • Groth, H.L.1    Norlund, P.2
  • 14
    • 0343975157 scopus 로고    scopus 로고
    • Shape optimisation of bonded lap joints and crack repairs
    • accepted
    • Kaye, R. and Heller, M. Shape optimisation of bonded lap joints and crack repairs. Int. J. Adhesion Adhes., 2000 (accepted).
    • (2000) Int. J. Adhesion Adhes.
    • Kaye, R.1    Heller, M.2
  • 15
  • 16
    • 0343103492 scopus 로고
    • SES DI 0942, Defence Systems Division, Canadair Group, Bombardier Inc.
    • Martin, P. ECP 365 Y470 bulkhead beef-up. SES DI 0942, Defence Systems Division, Canadair Group, Bombardier Inc., 1995.
    • (1995) ECP 365 Y470 Bulkhead Beef-Up
    • Martin, P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.