Postbuckling of stiffened panels using strut, strip, and finite element methods

AIAA Journal

Volumn 41, Issue 6, 2003, Pages 1172-1179

  Lillico, M ^a,c   Butler, R ^a   Hunt, G W ^a   Watson, A ^b   Kennedy, D ^b  

^a University of Bath   (United Kingdom)

^b CARDIFF UNIVERSITY   (United Kingdom)

^c AIRBUS OPERATIONS LTD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; BUCKLING; COMPRESSION TESTING; COMPUTER AIDED DESIGN; COMPUTER SIMULATION; DYNAMIC LOADS; ELASTICITY; FINITE ELEMENT METHOD;

EXACT STRIP THEORY; SOFTWARE PACKAGE VICONOPT; STIFFENED PANELS; STRUT THEORY;

AIRFRAMES;

EID: 0037934293     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2061     Document Type: Article

References (16)

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