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Volumn 63, Issue 1-3, 1997, Pages 384-394

Fiber metal laminates: An advanced material for future aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CORROSION RESISTANCE; COST EFFECTIVENESS; FATIGUE OF MATERIALS; FIRE RESISTANCE; MANUFACTURE; METALS;

EID: 0030736895     PISSN: 09240136     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0924-0136(96)02652-0     Document Type: Article
Times cited : (335)

References (19)
  • 5
    • 0018689720 scopus 로고
    • Fatigue properties of adhesive-bonded laminated sheet material of aluminium alloy
    • Schijve J., Lipzig H. van, Gestel G., Hoeymaker A. 'Fatigue properties of adhesive-bonded laminated sheet material of aluminium alloy', Engineering Fracture Mechanics, Vol. 12 (1979), pp 561-579
    • (1979) Engineering Fracture Mechanics , vol.12 , pp. 561-579
    • Schijve, J.1    Van Lipzig, H.2    Gestel, G.3    Hoeymaker, A.4
  • 10
    • 0040926934 scopus 로고
    • Damage tolerance aspects of an experimental Arall F-27 lower wing skin panel
    • Seven Springs
    • Veggel L. van. 'Damage Tolerance Aspects of an Experimental Arall F-27 Lower Wing Skin Panel', Arall users conference, Seven Springs (1987)
    • (1987) Arall Users Conference
    • Van Veggel, L.1
  • 14
    • 0011239462 scopus 로고
    • Feasibility study of the application of glare materials in ide body aircraft fuselage
    • Hamburg
    • Ohrloff N. and Horst P., 'Feasibility Study of the Application of Glare materials in ide Body Aircraft Fuselage', 13th European Chapter Conference of SAMPE, Hamburg (1992)
    • (1992) 13th European Chapter Conference of SAMPE
    • Ohrloff, N.1    Horst, P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.