TY - JOUR
T1 - 端壁抽吸控制下攻角对压气机叶栅叶尖泄漏流动的影响
AU - Zhang, Botao
AU - Liu, Bo
AU - Wang, Hejian
N1 - Publisher Copyright:
© 2020, Editorial Department of Journal of Aerospace Power. All right reserved.
PY - 2020/11
Y1 - 2020/11
N2 - In order to reduce the tip leakage loss and improve the tip passage blockage caused by the tip leakage vortex, numerical simulation was conducted to investigate the flow control effect of suction scheme with endwall slot in flow direction on the tip leakage flow in a diffuser cascade. The impact of incidence angle on flow control effect was analysed emphatically. Results showed that the leakage vortex intensity and the leakage loss were reduced by the endwall suction scheme by directly controlling the development of the tip leakage flow. The influence of endwall suction on the cascade flow field at the design and negative incidence angles was limited to the vicinity of the blade tip. However, at a large incidence angle, suction can advance the boundary layer separation in the low span region, and the position of the vortex shedding on the suction surface of blade raised to about 70% span. Therefore, the overall impact of the endwall suction scheme on the cascade at a large incidence angle was determined by both the reduction of leakage loss and the increase of separation loss. With the suction flow rate of 0.7%, the overall total pressure loss coefficient of aspirated cascade decreased by about 9.0%, 10.8% and 6.8%, respectively, at the incidence angles of -8°, 0°and +4°, and increased by about 5.7% at the incidence angles of +8°.
AB - In order to reduce the tip leakage loss and improve the tip passage blockage caused by the tip leakage vortex, numerical simulation was conducted to investigate the flow control effect of suction scheme with endwall slot in flow direction on the tip leakage flow in a diffuser cascade. The impact of incidence angle on flow control effect was analysed emphatically. Results showed that the leakage vortex intensity and the leakage loss were reduced by the endwall suction scheme by directly controlling the development of the tip leakage flow. The influence of endwall suction on the cascade flow field at the design and negative incidence angles was limited to the vicinity of the blade tip. However, at a large incidence angle, suction can advance the boundary layer separation in the low span region, and the position of the vortex shedding on the suction surface of blade raised to about 70% span. Therefore, the overall impact of the endwall suction scheme on the cascade at a large incidence angle was determined by both the reduction of leakage loss and the increase of separation loss. With the suction flow rate of 0.7%, the overall total pressure loss coefficient of aspirated cascade decreased by about 9.0%, 10.8% and 6.8%, respectively, at the incidence angles of -8°, 0°and +4°, and increased by about 5.7% at the incidence angles of +8°.
KW - Endwall suction
KW - Entropy analysis
KW - Flow control technique
KW - Incidence angle
KW - Leakage vortex
KW - Tip leakage flow
UR - http://www.scopus.com/inward/record.url?scp=85098149869&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.2020.11.017
DO - 10.13224/j.cnki.jasp.2020.11.017
M3 - 文章
AN - SCOPUS:85098149869
SN - 1000-8055
VL - 35
SP - 2400
EP - 2412
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 11
ER -