Experimental studies have been presented in this paper on dissimilar material metal/fibre laminates to investigate the fatigue response under tension-tension loading. The testing was evaluated on single lap joints (SLJs) with different joint technique; fastener bolted, adhesive bonded and hybrid (combination of bolted and bonded) joint with dimension of 160 mm length, 40 mm width and 3±0.5 mm thickness. The dynamic testing were subjected into constant frequency and stress ratio of 5 Hz and 0.1, respectively. The range of applied load level were defined in between 30 % to 90%. Theoretically, significant improvements in fatigue strength can be obtained by adopting long overlap length which used in the study, 64 mm. From the experimental study, the hybrid joint of dissimilar material reached highest load cycles followed by adhesive bonded and bolted joint.
