The Performance of the Self-Supplying Vortex Generator Jets on a High-Speed Compressor Cascade

References

1 Sasaki T, Breugelmans F. Comparison of sweep and dihedral effects on compressor cascade performance. J Turbomach 1998;120(3):454–63.10.1115/1.2841738Search in Google Scholar

2 Neshat MA, Akhlaghi M, Fathi A, Khaledi H. Investigating the effect of blade sweep and lean in one stage of an industrial gas turbine’s transonic compressor. Propul Power Res 2015;4(4):221–9.10.1016/j.jppr.2015.11.002Search in Google Scholar

3 Poehler T, Gier J, Jeschke P. Numerical and experimental analysis of the effects of non-axisymmetric contoured stator endwalls in an axial turbine. In: Proceeding of ASME Turbo Expo, Glasgow, UK, 2010.10.1115/GT2010-23350Search in Google Scholar

4 Ito Y, Watanabe T, Himeno T. Effect of endwall contouring on flow instability of transonic compressor. Int J Gas Turb Propul Power Syst 2008;2(1):24–9.10.38036/jgpp.2.1_24Search in Google Scholar

5 Snedden G, Dunn D, Ingram G, Gregory-Smith D. The performance of a generic non-axisymmetric end wall in a single stage, rotating turbine at on and off-design conditions. In: Proceeding of ASME Turbo Expo, Glasgow, UK, 2010.10.1115/GT2010-22006Search in Google Scholar

6 Nerger D, Saathoff H, Radespiel R, Gümmer V, Clemen C. Experimental investigation of endwall and suction side blowing in a highly loaded compressor stator cascade. J Turbomach 2012;134(2):021010.10.1115/1.4003254Search in Google Scholar

7 Xiaoqing Q, Songtao W, Guotai F, Zhongqi W. Aerodynamic design and analysis of a low-reaction axial compressor stage. Chinese J Aeronaut 2008;21(1):1–7.10.1016/S1000-9361(08)60001-1Search in Google Scholar

8 Yangwei L, Jinjing S, Lingpeng L. Corner separation control by boundary layer suction applied to a highly loaded axial compressor cascade. Energies 2014;7:7994–8007.10.3390/en7127994Search in Google Scholar

9 Yanming L, Jingjun Z, Haibin L, Songtao W. The influence of endwall wing fence length on secondary flow in compressor cascade. J Aerosp Power 2004;5:017.Search in Google Scholar

10 Jingjun Z, Jiang H, Yanming L, Fu T. Numerical simulation of endwall fence on the secondary flow in compressor cascade. In: Proceeding of ASME Turbo Expo 2008, Berlin, Germany, 2008.Search in Google Scholar

11 Ortmanns J, Pixberg C, Gümmer V. Numerical investigation of vortex generators to reduce cross-passage flow phenomena in compressor. Proc Inst Mech Eng Part A: J Power Energy 2011;225:877–85.10.1177/0957650911414323Search in Google Scholar

12 Hergt A, Meyer R, Engel K, Hergt A, Meyer R. Effects of vortex generator application on the performance of a compressor cascade. J Turbomach 2013;135(2):21–6.10.1115/GT2010-22464Search in Google Scholar

13 Braunscheidel EP, Culley DE, Zaman KB. Application of synthetic jets to reduce stator flow separation in a low speed axial compressor. In: Proceeding of AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 2008.10.2514/6.2008-602Search in Google Scholar

14 Yanping S, Huanlong C, Fu C, Zhongqi W. Effects of air injection on performance of highly-loaded compressor cascades. In: Proceeding of ASME Turbo Expo, Montreal, Canada, 2007.Search in Google Scholar

15 Dongmin F, Fu C, Yanping S, Huanlong C, Zhongqi W. Enhancing aerodynamic performances of highly loaded compressor cascades via air injection. Chinese J Aeronaut 2009;22(2):121–8.10.1016/S1000-9361(08)60077-1Search in Google Scholar

16 Терещенко Ю М. Influence of improvements of the cascade’s aerodynamic performance on compressor’s characteristic performance. Beijing: China Machine Press, 1984.Search in Google Scholar

17 Hong L, Daomao X. The validity of hole configurations on the aerodynamic performance of turbine blade. J Eng Thermodyn 2008;05:63–766. (In Chinese)Search in Google Scholar

18 Yanping S, Fu C, Guijie Z, Kaiying C, Zhongqi W. Numerical investigation of boundary layer suction in compressor cascade with large turning angles. J Aerosp Power 2005;20(4):561–6.Search in Google Scholar

19 Min Z, Rugen W, Lingjun Z, Yingwu Z. Effect of slot width on the aerodynamic performance of compressor cascade. J Aerosp Power 2008;23(06):1077–81.Search in Google Scholar

20 Min Z, Rugen W, Zhaohui C, Xiangyi Z. Research on effect of slot inlet angle and turning angle on the flow field characteristic of cascade. J Aerosp Power 2008;23(1):125–9.Search in Google Scholar

21 Culley DE, Bright MM, Prahst PS, Strazisar AJ. Active flow separation control of a stator vane using surface injection in a multistage compressor experiment. In: Proceeding of ASME Turbo Expo, Atlanta, Georgia, 2003.10.1115/GT2003-38863Search in Google Scholar

22 Wiederhold O, Hecklau M, King R, Nitsche W, Huppertz A, Swoboda M. Multivariable control in a critically loaded compressor cascade. Int J Flow Control 2011;2(4):219–36.10.1260/1756-8250.2.4.219Search in Google Scholar

23 Hecklau M, Wiederhold O, Zander V, King R, Nitsche W, Huppertz A, et al.. Active separation control with pulsed jets in a critically loaded compressor cascade. AIAA J 2011;49(8):1729–39.10.2514/1.J050931Search in Google Scholar

24 Zander V, Nitsche W. Control of secondary flow structures on a highly loaded compressor cascade. Proc Inst Mech Eng Part A: J Power Energy 2013;227(6):674–82.10.1177/0957650913495538Search in Google Scholar

25 Evans S, Hodson H, Hynes T, Wakelam C, Hiller SJ. Controlling separation on a simulated compressor blade using vortex-generator jets. J Propul Power 2010;26(4):819–27.10.2514/1.45518Search in Google Scholar

26 Huaping L, Huanlong C, Deying L, Yujie G, Xiaoqi C, Fu C. Secondary flow control in high-turning compressor cascade using vortex generator jet. J Aerosp Power 2015;30(4):838–45.Search in Google Scholar

27 Yanyan F, Yanping S, Huaping L, Fu C. Effects of end-wall vortex generator jet on flow separation control in compressor cascade under different angles of attack. J Propul Technol 2015;36(1):54–60. (In Chinese)Search in Google Scholar

28 Milanovic IM, Zaman MQ. Fluid dynamics of highly pitched and yawed jets in crossflow. AIAA J 2004;42(5):874–82.10.2514/1.2924Search in Google Scholar

29 Krzysiak A. Control of flow separation using self-supplying air-jet vortex generators. AIAA J 2008;46(9):2229–34.10.2514/1.30150Search in Google Scholar

30 Hergt A, Meyer R, Liesner K, Nicke E. A new approach for compressor endwall contouring. In: Proceeding of ASME Turbo Expo, Vancouver, British Columbia, Canada, 2011.10.1115/GT2011-45858Search in Google Scholar

31 Compton DA, Johnston JP. Streamwise vortex production by pitched and skewed jets in a turbulent boundary layer. AIAA J 1992;30(3):640–7.10.2514/3.10967Search in Google Scholar

32 Khan ZU. On the dominant vortex created by a pitched and skewed jet in crossflow. Stanford University, 1999.Search in Google Scholar

33 Selby GV, Lin JC, Howard FG. Control of low-speed turbulent separated flow using jet vortex generators. Exp Fluids 1992;12(6):394–400.10.1007/BF00193886Search in Google Scholar

34 Zhang X, Collins MW. Nearfield evolution of a longitudinal vortex generated by an inclined jet in a turbulent boundary layer. ASME J Fluids Eng 1997;119(4):934–9.10.1115/1.2819520Search in Google Scholar

35 Florian VS, Stefan W, Arne V, et al. Evaluation and parameterization of round vortex generator jet experiments for flow control. AIAA J 2012;50(11):2508–24.10.2514/1.J051694Search in Google Scholar

36 Xiaochen M, Bo L, Zhiyuan C, Peng Z. Research on corner separation control for compressor cascade with end-wall jet flow. J Propul Tech 2014;35(12):1615–162. (In Chinese)Search in Google Scholar

37 Evans S, Coull J, Haneef I, Hodson H. Minimizing the loss produced by a turbulent separation using vortex generator jets. AIAA J 2012;50(4):778–87.10.2514/1.J050790Search in Google Scholar

38 Stillfried FV, Wallin S, Johansson AV, Casper M, Ortmanns J. Evaluation and parameterization of round vortex generator jet experiments for flow control. AIAA J 2012;50(11):2508–24.10.2514/1.J051694Search in Google Scholar