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Materials and Design
Volumn 27, Issue 1, 2006, Pages 10-20
Design case study for a comparative performance analysis of aerospace materials
Author keywords

E. Fatigue; H. Selection for material properties; I. Buckling
Indexed keywords

AIRCRAFT; ALUMINUM; CARBON FIBER REINFORCED PLASTICS; CORRELATION THEORY; COSTS; FUSELAGES; LIFE CYCLE; PRODUCT DEVELOPMENT; STIFFNESS;
EID: 23444446308     PISSN: 02613069     EISSN: 18734197     Source Type: Journal    
DOI: 10.1016/j.matdes.2004.09.022     Document Type: Article
Times cited : (9)
References (13)
  • 1
    • 84903374288 scopus 로고    scopus 로고
    • Aircraft structures in the century ahead
    • Dutch Royal Society of Aeronautics
    • Beukers A, Tooren MJLvan, Vermeeren CAJR. Aircraft structures in the century ahead. Dutch Royal Society of Aeronautics
    • Beukers, A.1    van Tooren, M.J.L.2    Vermeeren, C.A.J.R.3
  • 2
    • 33644478342 scopus 로고
    • CRACKS - A computer program for the damage tolerance analysis of fuselage panels
    • Delft University of Technology
    • M. Bos CRACKS - a computer program for the damage tolerance analysis of fuselage panels Delft University of Technology 1988
    • (1988)
    • Bos, M.1
  • 4
    • 14544273813 scopus 로고
    • The compressive properties of glare
    • Delft, Faculty of Aerospace Engineering LR-666
    • Verolme JL. The compressive properties of glare. Delft, Faculty of Aerospace Engineering LR-666; 1991
    • (1991)
    • Verolme, J.L.1
  • 6
    • 0042988499 scopus 로고    scopus 로고
    • Review of damage tolerance for composite sandwich airframe structures
    • DOT/FAA/AR-99/49
    • Tomblin J, et al. Review of damage tolerance for composite sandwich airframe structures. DOT/FAA/AR-99/49; 1999
    • (1999)
    • Tomblin, J.1
  • 7
    • 0004030341 scopus 로고    scopus 로고
    • Composite airframe structures
    • Hong Kong
    • Niu MCY. Composite airframe structures. Hong Kong, 1996
    • (1996)
    • Niu, M.C.Y.1
  • 8
    • 0004000511 scopus 로고
    • A summary of diagonal tension, part 1 - Methods of analysis, NACA TN-2661
    • Washington
    • Kuhn P, Peterson JP, Levin L. A summary of diagonal tension, part 1 - methods of analysis, NACA TN-2661. Washington: 1952
    • (1952)
    • Kuhn, P.1    Peterson, J.P.2    Levin, L.3
  • 10
    • 33644480685 scopus 로고
    • Residual strength analysis of structures in aluminium alloy and fibre metal laminates
    • Delft: Meinema B.V. Delft
    • K.J.J.M. Zaal Residual strength analysis of structures in aluminium alloy and fibre metal laminates 1995 Meinema B.V. Delft Delft
    • (1995)
    • Zaal, K.J.J.M.1
  • 11
    • 0021599497 scopus 로고
    • Fracture analysis of stiffened structure, damage tolerance of metallic structures: Analysis methods and applications
    • ASTM STP 842. Chang, JB, Rudd JL. American Society for Testing and Materials
    • Swift T. Fracture analysis of stiffened structure, damage tolerance of metallic structures: Analysis methods and applications. ASTM STP 842. Chang, JB, Rudd JL. American Society for Testing and Materials; 1984. p. 69-107
    • (1984) , pp. 69-107
    • Swift, T.1
  • 12
    • 33644477951 scopus 로고    scopus 로고
    • Compression response of a keel panel with and without damage
    • NASA TM-110302 Hampton: Langley Research Center
    • D.M. McGowan D.R. Ambur Compression response of a keel panel with and without damage, NASA TM-110302 1997 Langley Research Center Hampton
    • (1997)
    • McGowan, D.M.1    Ambur, D.R.2

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.