Predicting impact damage of composite stiffened panels

Aeronautical Journal

Volumn 104, Issue 1032, 2000, Pages 97-103

  Davies, G A O ^a   Zhang, X ^b  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; BUCKLING; DELAMINATION; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; MATHEMATICAL MODELS; STIFFNESS;

DEBONDING; LAMINATED CARBON EPOXY COMPOSITES; POSTBUCKLING STRENGTH;

AIRCRAFT MATERIALS;

EID: 0033886720     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (16)

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