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Volumn 20, Issue 1, 2000, Pages 39-45

Stiffness behaviour due to fracture in adhesively bonded composite-to-aluminum joints: I. Theoretical model

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; BOND STRENGTH (MATERIALS); DEFLECTION (STRUCTURES); FINITE ELEMENT METHOD; FRACTURE; MATHEMATICAL MODELS; REINFORCED PLASTICS; STIFFNESS; STRESS ANALYSIS; TENSILE STRESS;

EID: 0033905753     PISSN: 01437496     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0143-7496(99)00013-5     Document Type: Article
Times cited : (55)

References (14)
  • 5
    • 0000507109 scopus 로고    scopus 로고
    • Tong L. AIAA J. 36(3):1998;448.
    • (1998) AIAA J , vol.36 , Issue.3 , pp. 448
    • Tong, L.1
  • 7
    • 85031589414 scopus 로고
    • Stiffness change as a non-destructive damage measurement
    • US Army Research and Technology Laboratories (AVRADCOM), NASA Langley Research Center Hampton, VA, 23665
    • O'Brien TK. Stiffness change as a non-destructive damage measurement. Structures Laboratory Report, US Army Research and Technology Laboratories (AVRADCOM), NASA Langley Research Center Hampton, VA, 23665, 1979.
    • (1979) Structures Laboratory Report
    • O'Brien, T.K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.