2023/6/7 0:00:00 YANG Yun, LIN Zening, HONG Yang, JIANG Tao, SHANG Jianzhong, LUO Zirong 8true r, and the change of the flow field parameters along the segment radial was ignored. Therefore, the annular cascade segment can be considered as a planar cascade, and the periodic inflow is considered based on the interaction between the planar cascade and the harmonic wave. The unsteady excitation force of the interaction line spectrum between the front guide vane segment and the rotor segment is derived. The unsteady thrust line spectrum prediction formula is obtained through the circumferential integration of the rotor segment. The validity of the formula is verified through numerical and experimental methods. A design parameter impact analysis was conducted, and it was found that when the ratio of the current guide vane rotor spacing to the chord length of the front guide vane is greater than 1, the rotor rear guide vane spacing has almost no impact on the excitation force line spectrum thrust of a single rotor blade.]]> 2023/6/7 9:08:55 HE Shengyang, WU Xingyu, WEI Yingsan, JIN Shuanbao, ZHAI Shuo, CHENG Gong 7true 2023/6/7 9:08:55 QIAO Mingzhong, LU Xihao, ZHANG Chi 6true 2023/6/7 9:08:55 YU Fei, FAN Qingchuan, XUAN Min 5true 2023/6/7 9:08:55 WEI Keke, GAO Xiaopeng, MA Cheng, DONG Zushun 4true 2023/6/7 9:08:55 ZHOU Wei, LI Yiying, CHEN Shuhui, DIND Bo 3true 2023/6/7 9:08:56 LI Haiyan, CHAO Yanjing, LI Haijiang, GUO Lei, LI Hongsong 2true 2023/6/7 9:08:56 CHEN Xijiang, LIANG Quanen, HAN Xianquan, AN Qing 1true