The application of residual stress tailoring of snap-through composites for variable sweep wings

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 7, Issue , 2006, Pages 4607-4618

  Mattioni, F ^a,b,c   Gatto, A ^a,b   Weaver, P M ^a,b,c   Friswell, M I ^a,b,c   Potter, K D ^a,b  

^a UNIVERSITY OF BRISTOL   (United Kingdom)

^b Queen's Building ^*  (United Kingdom)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING STRENGTH; CARBON FIBER REINFORCED PLASTICS; CURING; METHOD OF MOMENTS; RESIDUAL STRESSES; STRESS ANALYSIS; TRUSSES;

BENDING STRESSES; MOMENT OF INERTIA; RIBS; UNSYMMETRIC STACK SEQUENCE; VARIABLE SWEEP WINGS;

COMPOSITE MATERIALS;

EID: 34247124246     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1972     Document Type: Conference Paper

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