Fig. 10 | Scientific Reports

Fig. 10

From: Failure analysis and size optimization of CFRP composite single-lap bonded joints based on the influence of multiple parameters

Fig. 10

The peel stress S33 and the shear stress S13 distribution of adhesive at different loading points, (a) S33 of 1.0-FF-S1-W25-L50 and 0.5-PF-S1-W25-L65;(b) S13 of 1.0-FF-S1-W25-L50 and 0.5-PF-S1-W25-L65; (c) S33 of 0.5-FF-S1-W50-L12 and 0.5-PF-S1-W20-L12;(d) S13 of 0.5-FF-S1-W50-L12 and 0.5-PF-S1-W20-L12; (e) S33 of 1.0-FF-S2-W25-L30 and 1.0-FF-S2-W30-L12; (f) S33 of 1.0-FF-S2-W25-L30 and 1.0-FF-S2-W30-L12.

Back to article page