Numerical investigations of an imperfect stringer-stiffened composite wing torsion box - An analysis concept

Composites Part B: Engineering

Volumn 27, Issue 1, 1996, Pages 59-69

  Skrna Jakl, I C ^a   Stiftinger, M A ^a   Rammerstorfer, F G ^a  

^a VIENNA UNIVERSITY OF TECHNOLOGY   (Austria)

Author keywords

Buckling; Finite element; Stringer stiffened; Wing torsion box

Indexed keywords

BUCKLING; CALCULATIONS; DELAMINATION; FAILURE (MECHANICAL); FINITE ELEMENT METHOD; STABILITY; STRESSES; STRUCTURAL ANALYSIS; WINGS;

FIRST PLY FAILURE CALCULATION; GEOMETRICAL IMPERFECTION; GLOBAL LOCAL APPROACH; INTERLAMINAR STRESSES; LOAD DEFLECTION CURVE; POSTBUCKLING BEHAVIOUR; STRINGER STIFFENED COMPOSITE; WING TORSION BOX;

COMPOSITE STRUCTURES;

EID: 0029777233     PISSN: 13598368     EISSN: None     Source Type: Journal    
DOI: 10.1016/1359-8368(95)00007-0     Document Type: Article

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