“…As illustrated in Figure 2, the polymer composite bolted T-joint with configuration (hereafter abbreviated as conventional T-joint) consists of two L ers, a bottom layer, a triangle filling area and outer wrapped skin, where L-s and base panel layers are composite laminates, and the triangle filling area m of resin matrix, short fibers, or twisted fibers [6]. When transverse bending lo mitted to the corner area of the T-joint, due to the significantly lower inte chanical properties of composite materials compared to that is in-plane [7] tional T-joint may experience failure modes such as bonding interface fail delamination, and random crack propagation within the triangle filling area to improve the load-carrying capacity of the conventional T-joint, some rese adopted methods such as stitching [9][10][11][12], Z-pin [13][14][15], and triangle filling a ment [1,16,17] to delay the failure in interlaminar and triangle filling are stitching and Z-pins can effectively delay and reduce delamination damag and improve its load-carrying capacity [18], but they may also weaken the chanical properties of laminates [19][20][21]. Moreover, the filling material in the is still connected to the L-shaped layer through the resin matrix, and the tr area remains a weak position for bearing load, thus the degree of improv mechanical performances of joints by this method is limited [17].…”