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Volumn 61, Issue 13, 2001, Pages 1841-1852

Buckling behaviour and delamination growth in impacted composite specimens under fatigue load: An experimental study

Author keywords

B. Fatigue; B. Impact behaviour; C. Buckling; C. Delamination; D. Ultrasonics

Indexed keywords

BUCKLING; CARBON FIBERS; CYCLIC LOADS; DELAMINATION; FATIGUE TESTING; ULTRASONIC TESTING;

EID: 0035477263     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0266-3538(01)00085-9     Document Type: Article
Times cited : (57)

References (30)
  • 3
    • 0020993322 scopus 로고
    • Effect of low-velocity impact damage on the fatigue behavior of graphite/epoxy laminates
    • (1983) ASTM STP , vol.813 , pp. 116-135
    • Ramkumar, R.L.1
  • 18
    • 0003249161 scopus 로고    scopus 로고
    • Residual strength of composite aircraft structures with damage
    • fatigue and fracture (USA). ASM International
    • (1996) ASM Handbook , vol.19 , pp. 920-935
    • Poe C.C., Jr.1
  • 22
    • 0003921886 scopus 로고    scopus 로고
    • Optical whole field measurement techniques for mechanical testing - A
    • The Aeronautical Research Institute of Sweden
    • (1999) FFA TN 1999-35
    • Melin, L.G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.