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      KCI등재 SCIE SCOPUS

      Secondary flow control using endwall jet fence in a high-speed compressor cascade

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      https://www.riss.kr/link?id=A105082145

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      다국어 초록 (Multilingual Abstract)

      This paper proposes a secondary flow control concept using Endwall jet fence (EJF). A parametric investigation concerning the variations of the jet location along the axial and pitch-wise direction as well as the skew angle is conducted numerically to...

      This paper proposes a secondary flow control concept using Endwall jet fence (EJF). A parametric investigation concerning the variations of the jet location along the axial and pitch-wise direction as well as the skew angle is conducted numerically to validate the potential of EJF in a high-speed compressor cascade with an inlet Mach number of 0.67. And then the interaction mechanisms between the EJF and the endwall secondary flow are discussed in detail. The results show that the EJF could reduce the corner separation and losses significantly by inputting transverse momentum component, inducing a concentrated jet vortex to block the pitch-wise migration of the passage vortex as well as enhancing the energy exchange between the endwall boundary layer and the mainstream. The jet location and the skew angle are important for the influence of EJF on the cascade performance. In this work, a maximum total pressure loss reduction of 11.6 % is obtained by the EJF located at 30 % of the axial chord and 10 % of the pitch with a skew angle of β = 40°, whereas the jetto-inflow mass flow ratio is only about 0.4 %, validating the high efficiency of this flow control concept. For the off-design points, the EJF also shows appreciable potential on the endwall secondary flow control and loss reduction.

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      참고문헌 (Reference)

      1 A. Hergt, "new approach for compressor endwall contouring" 2011

      2 G. Snedden, "The performance of a generic non-axisymmetric end wall in a single stage, rotating turbine at on and off-design conditions" 2010

      3 Y. M. Liu, "The influence of endwall wing fence length on secondary flow in compressor cascade" 19 (19): 666-670, 2004

      4 임병준, "Stall inception and warning in a single-stage transonic axial compressor with axial skewed slot casing treatment" 대한기계학회 28 (28): 3569-3581, 2014

      5 T. Kawai, "Secondary flow control and loss reduction in a turbine cascade using endwall fences" 32 : 375-387, 1989

      6 X. C. Mao, "Research on corner separation control for compressor cascade with endwall jet flow" 35 (35): 1615-1622, 2014

      7 J. J. Zhong, "Numerical simulation of endwall fence on the secondary flow in compressor cascade" 2008

      8 Jinlan Gou, "Numerical investigation on the effects of real industrial bleeding geometry in a high-speed compressor stage" 대한기계학회 30 (30): 5275-5286, 2016

      9 J. Ortmanns, "Numerical investigation of vortex generators to reduce cross-passage flow phenomena in compressor" 225 : 877-885, 2011

      10 T. Poehler, "Numerical and experimental analysis of the effects of non-axisymmetric contoured stator endwalls in an axial turbine" 2010

      1 A. Hergt, "new approach for compressor endwall contouring" 2011

      2 G. Snedden, "The performance of a generic non-axisymmetric end wall in a single stage, rotating turbine at on and off-design conditions" 2010

      3 Y. M. Liu, "The influence of endwall wing fence length on secondary flow in compressor cascade" 19 (19): 666-670, 2004

      4 임병준, "Stall inception and warning in a single-stage transonic axial compressor with axial skewed slot casing treatment" 대한기계학회 28 (28): 3569-3581, 2014

      5 T. Kawai, "Secondary flow control and loss reduction in a turbine cascade using endwall fences" 32 : 375-387, 1989

      6 X. C. Mao, "Research on corner separation control for compressor cascade with endwall jet flow" 35 (35): 1615-1622, 2014

      7 J. J. Zhong, "Numerical simulation of endwall fence on the secondary flow in compressor cascade" 2008

      8 Jinlan Gou, "Numerical investigation on the effects of real industrial bleeding geometry in a high-speed compressor stage" 대한기계학회 30 (30): 5275-5286, 2016

      9 J. Ortmanns, "Numerical investigation of vortex generators to reduce cross-passage flow phenomena in compressor" 225 : 877-885, 2011

      10 T. Poehler, "Numerical and experimental analysis of the effects of non-axisymmetric contoured stator endwalls in an axial turbine" 2010

      11 O. Wiederhold, "Multivariable control in a critically loaded compressor cascade" 2 (2): 219-236, 2011

      12 M. A. Neshat, "Investigating the effect of blade sweep and lean in one stage of an industrial gas turbine ׳s transonic compressor" 4 (4): 221-229, 2015

      13 Juan Du, "Initial selection of groove location combination for multi-groove casing treatments" 대한기계학회 30 (30): 697-704, 2016

      14 D. Nerger, "Experimental investigation of endwall and suction side blowing in a highly loaded compressor stator cascade" 134 (134): 255-267, 2012

      15 F. V. Stillfried, "Evaluation and parameterization of round vortex generator jet experiments for flow control" 50 (50): 2508-2524, 2012

      16 H. P. Liu, "Endwall secondary flow control in a high-speed compressor cascade with vortex generator jets" 2010

      17 H. P. Liu, "Effects of vortex generator jet on corner separation/stall in high-turning compressor cascade" 22 : 555-562, 2016

      18 Y. Ito, "Effect of endwall contouring on flow instability of transonic compressor" 2 (2): 24-29, 2008

      19 L. Yangwei, "Corner separation control by boundary layer suction applied to a highly loaded axial compressor cascade" 7 : 7994-8007, 2014

      20 V. Zander, "Control of secondary flow structures on a highly loaded compressor cascade" 227 (227): 674-682, 2013

      21 G. V. Selby, "Control of lowspeed turbulent separated flow using jet vortex generators" 12 : 394-400, 1992

      22 T. Sasaki, "Comparison of sweep and dihedral effects on compressor cascade performance" 120 (120): 454-463, 1998

      23 X. Q. Qian, "Aero-dynamic design and analysis of a low-reaction axial compressor stage" 21 (21): 1-7, 2008

      24 M. Hecklau, "Active separation control with pulsed jets in a critically loaded compressor cascade" 49 (49): 1729-1739, 2011

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2012-11-05 학술지명변경 한글명 : 대한기계학회 영문 논문집 -> Journal of Mechanical Science and Technology KCI등재
      2010-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2008-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-19 학술지명변경 한글명 : KSME International Journal -> 대한기계학회 영문 논문집
      외국어명 : KSME International Journal -> Journal of Mechanical Science and Technology
      KCI등재
      2006-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2004-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2001-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      1998-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      2016 1.04 0.51 0.84
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.74 0.66 0.369 0.12
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