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, Adapter jig for impact machines. (b) Block shear impact test specimens
, 19 4 Stress distributions in the adhesive (extracted from h = {?e, ?e/2, 0, e/2, e}) along the overlap and zoom on the associated edge effects near the right and left edges of the adhesive joint. (a) ? xx distributions. (b) ? yy distributions. (c) ? xy distributions
, (b) Chamfered beaks with different angles ? = {15 ?, p.30
, (c) Filleted beaks with different angles ? = {15 ?, p.30
, Shoulder filleted beaks with different shoulder thicknesses t = {0 mm, 0.1 mm, 0.2 mm}
, b) Results for the tensile-shear test (? = 45 ? ). (c) Results for the shear test (? = 90 ? ). (d) Results for the compression-shear test (? = 135 ?
, 25 10 Description of the ARCAN TCS finite element model. (a) Boundary conditions. (b) Global mesh. (c) Zoom on the mesh near the right edge of the adhesive joint, p.27
, The spatial vs temporal stress distributions in the mid-plane of the adhesive (extracted from h = 0) in the case of a tensile test for three configurations : (a-c) m = 1 kg and v= 10.75 m.s ?1 . (d-f) m = 10 kg and v= 3
, xx distributions. (b, e, h) ? yy distributions. (c, f, i) ? xy distributions, vol.28, p.15
, 29 14 Modal analysis of the ARCAN TCS specimen. (a) Tensile test (m = 10 kg, v= 3.4 m.s ?1 ). (b) Compression-shear test (m = 50 kg, v= 1.52 m.s ?1 ). (c) Compression-shear test (m = 1 kg, v= 10.75 m.s ?1 ), The spatial vs temporal stress distributions in the mid-plane of the adhesive (extracted from h = 0) in the case of a compression-shear test for three configurations : (a-c) m = 1 kg and v= 10
, Main excited vibration modes. (a) Tensile loading. (b-d) Compression-shear loading