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Volumn 38, Issue 23, 2004, Pages 2133-2142

An investigation into an advanced composite finite element explicit biphase model: Part II - Damage parameters

Author keywords

Advanced aerospace composite structures; Damage tolerance; Dynamic response; Explicit biphase solver; Impact

Indexed keywords

AEROSPACE INDUSTRY; AIRCRAFT; COMPOSITE STRUCTURES; DEFECTS; DYNAMIC LOADS; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; IMPACT TESTING; MATHEMATICAL MODELS; PARAMETER ESTIMATION; POISSON RATIO; SENSITIVITY ANALYSIS;

EID: 10644258763     PISSN: 00219983     EISSN: None     Source Type: Journal    
DOI: 10.1177/0021998304045587     Document Type: Article
Times cited : (2)

References (6)
  • 4
    • 0035308326 scopus 로고    scopus 로고
    • Numerical investigation of a crash test of a composite helicopter subfloor structure
    • McCarthy, M.A. and Wiggenraad, J.F.M. (2001). Numerical Investigation of a Crash Test of a Composite Helicopter Subfloor Structure, Composite Structures, 51: 345-359.
    • (2001) Composite Structures , vol.51 , pp. 345-359
    • McCarthy, M.A.1    Wiggenraad, J.F.M.2
  • 6
    • 10644261813 scopus 로고    scopus 로고
    • An investigation into an advanced composites explicit Bi-phase model
    • Royal Aeronautical Society and the Institution of Engineers, Brisbane, Australia
    • Bayandor, J., Thomson, R.S. and Scott, M.L. (2003). An Investigation into an Advanced Composites Explicit Bi-phase Model, In: Proceedings of the 10th Australian International Aerospace Congress (AIAC-10), Royal Aeronautical Society and the Institution of Engineers, Brisbane, Australia.
    • (2003) Proceedings of the 10th Australian International Aerospace Congress (AIAC-10)
    • Bayandor, J.1    Thomson, R.S.2    Scott, M.L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.