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Volumn 523, Issue 1-2, 2009, Pages 118-124

The response of aluminium/GLARE hybrid materials to impact and to in-plane fatigue

Author keywords

Bonded hybrids; Damage tolerance; Fatigue crack growth; Fibre metal laminates; Impact

Indexed keywords

DAMAGE TOLERANCE; FATIGUE DAMAGE; GLARE; HIGH STRENGTH ALLOYS; HYBRID COMPOSITES; SCANNING ELECTRON MICROSCOPY;

EID: 69149107138     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.msea.2009.05.055     Document Type: Article
Times cited : (36)

References (42)
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  • 6
    • 85162827037 scopus 로고    scopus 로고
    • Aeronautics and Space
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    • Airworthiness Standard , Issue.PART 25
  • 7
    • 85162840883 scopus 로고    scopus 로고
    • Joint Aviation Requirements, JAR-25, Large Aeroplanes; Global Engineering Documents, on behalf of Joint Airworthiness Authorities Committees.
    • Joint Aviation Requirements, JAR-25, Large Aeroplanes; Global Engineering Documents, on behalf of Joint Airworthiness Authorities Committees.
  • 17
  • 28
    • 85162768863 scopus 로고
    • NASA TM-89013
    • W.S. Johnson, NASA TM-89013, 1986.
    • (1986)
    • Johnson, W.S.1
  • 32
    • 85162804406 scopus 로고    scopus 로고
    • MSc thesis, Cranfield University UK
    • F. Bagnoli, MSc thesis, Cranfield University (UK), 2006.
    • (2006)
    • Bagnoli, F.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.