TY - GEN
T1 - Investigation of the Impact of Relative Position on Corner Stall in Tandem Stators
AU - Zhang, Chuanhai
AU - Liu, Baojie
AU - Chen, Diyun
AU - Jiang, Zhuyu
AU - Yue, Shaoyuan
N1 - Publisher Copyright:
© Press of Acta Aeronautica et Astronautica Sinica 2026.
PY - 2026
Y1 - 2026
N2 - This study employs numerical simulations to investigate the impact of pitch relative positions (PP) and axial relative positions (AO) on tandem stator performance and corner stall. The results indicate that two distinct types of corner stall behavior are exhibited. With PP values of 0.50 and 0.60, the rear blade stalls first, while with values of 0.70 to 0.90, it is the front blade that stalls first. Additionally, there is a trend for corner stall to be delayed as PP value increases, which is attributed to PP changing the load distribution between front and rear blades. Corner stall is also delayed as AO increases. The mechanism is that the adverse pressure gradient of the suction surface boundary layer in the root regions decreases with AO increasing, which delays boundary layer separation. Investigations into tandem stators with various combinations of PP and AO show that the type of corner stall primarily correlates with changes of PP, and type of front blade corner stall first associates with wider operating range and lower losses. Considering both loss and stall margin, the optimal PP range for the tandem stator root is between 0.80 and 0.90, while the optimal AO range is between −0.05 and 0.
AB - This study employs numerical simulations to investigate the impact of pitch relative positions (PP) and axial relative positions (AO) on tandem stator performance and corner stall. The results indicate that two distinct types of corner stall behavior are exhibited. With PP values of 0.50 and 0.60, the rear blade stalls first, while with values of 0.70 to 0.90, it is the front blade that stalls first. Additionally, there is a trend for corner stall to be delayed as PP value increases, which is attributed to PP changing the load distribution between front and rear blades. Corner stall is also delayed as AO increases. The mechanism is that the adverse pressure gradient of the suction surface boundary layer in the root regions decreases with AO increasing, which delays boundary layer separation. Investigations into tandem stators with various combinations of PP and AO show that the type of corner stall primarily correlates with changes of PP, and type of front blade corner stall first associates with wider operating range and lower losses. Considering both loss and stall margin, the optimal PP range for the tandem stator root is between 0.80 and 0.90, while the optimal AO range is between −0.05 and 0.
KW - Axial relative position
KW - Corner stall
KW - High load
KW - Pitch relative position
KW - Subsonic
KW - Tandem stators
UR - https://www.scopus.com/pages/publications/105028355304
U2 - 10.1007/978-981-95-3037-3_8
DO - 10.1007/978-981-95-3037-3_8
M3 - 会议稿件
AN - SCOPUS:105028355304
SN - 9789819530366
T3 - Lecture Notes in Mechanical Engineering
SP - 112
EP - 131
BT - Proceedings of the 2nd Aerospace Frontiers Conference, AFC 2025 - Volume VI
PB - Springer Science and Business Media Deutschland GmbH
T2 - 2nd Aerospace Frontiers Conference, AFC 2025
Y2 - 11 April 2025 through 14 April 2025
ER -