Parametric analyses of stitched composite T-joints by the finite element method

Materials and Design

Volumn 23, Issue 8, 2002, Pages 751-758

  Stickler, P B ^a   Ramulu, M ^b  

^a BOEING COMPANY   (United States)

^b University of Washington   (United States)

Author keywords

Joining; Mechanical; Polymer matrix composites

Indexed keywords

BENDING STRENGTH; ELASTIC MODULI; INTERFACES (MATERIALS); LOADS (FORCES); STITCHING (METAL JOINING);

TRANSVERSE STITCHING;

FIBER REINFORCED MATERIALS;

COMPOSITE; JOINT; POLYMER;

EID: 0036920531     PISSN: 02641275     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0261-3069(02)00070-5     Document Type: Article

References (14)

1. A Parametric study of residual strength and stiffness for impact damaged composites
2. Parametric study of variables that affect fiber microbuckling initiation in composite laminates: Part 1 - Analyses
3. Parametric study of variables that affect fiber microbuckling initiation in composite laminates: Part 2-Experiments
4. Interlaminar fracture toughness of selectively stitched thick carbon fibre reinforced polymer fabric composite laminates
5. Local buckling of stitched composite laminates
6. Parametric study of the behavior of graphite-epoxy panels with stiffener terminations
7. Analytical prediction of damage growth in notched composite panels loaded in compression
8. Parametric study of interfacial debonding in adhesively bonded composite joints
9. Investigation of mechanical behavior of transverse stitched t-joints with PR520 resin in flexure and tension