The performance of post-buckled CFRP stringer-stiffened panels containing defects and damage

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

Volumn 4, Issue , 2003, Pages 2536-2546

  Greenhalgh, Emile ^a   Meeks, Charlotte ^b   Clarke, Andrew ^a   Thatcher, James ^a  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b QinetiQ   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; CRACK PROPAGATION; DEFECTS; FAILURE ANALYSIS; FRACTOGRAPHY; PERFORMANCE; STIFFNESS; STRAIN; STRENGTH OF MATERIALS; WINGS;

DAMAGE GROWTH; IMPACT DAMAGE; PANEL STRENGTH; SKIN-STIFFENER DEBONDING; SKIN-STRINGER PANEL;

CARBON FIBER REINFORCED PLASTICS;

EID: 0042011187     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Ireman T, 'Efficient Design and Verification of Composite Structures (EDAVCOS)', BRPR980611, Final Report, (2001).
2. Heath B, 'Advanced Structural Efficiency (ADSTREFF) - State of Art Report', BETC-1039, (2000)
3. Singh S & Greenhalgh E, 'Validation Data for the Development of Realistic Models of Delamination Growth in Composite Structures', EuroMECH Colloquium 400, Impact and Damage Tolerance Modelling of Composite Structures, Imperial College, London, (1999).
4. Greenhalgh E, Clarke A & Thatcher J, 'Mechanical Evaluation of Stringer-Stiffened Panels Tested Under Compression (Contribution to EDAVCOS D3.3.1)', DERA Technical Report, DERA/MSS/MSMA2/TR002079 (DERA.T3.TR.4), (2000)
5. Greenhalgh E, 'Summary of Test Definitions - EDAVCOS Deliverable D3.2.2', DERA/MSS/MSMA2 TR002081, DERA.T3.TR.3, (2000).
6. Wiggenraad J, Greenhalgh E & Olsson, R, 'Design and Analysis of Stiffened Composite Panels for Damage Resistance and Tolerance', WCCM V, Fifth World Congress on Computational Mechanics, Vienna, Austria, July 7-12, (2002).
7. Meeks C, Greenhalgh E & Van Rijn J, 'Mechanisms of Stiffener Debonding in Post-Buckled CFRP Aerospace Panels', Submitted to Composites A, (2002).