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Pre-swirl Nozzle Geometry Optimization to Increase Discharge Coefficient Using CFD Analysis

Pre-swirl system의 유량계수 향상을 위한 Pre-swirl nozzle의 형상 최적화 전산해석 연구

  • Lee, Hyungyu (Department of Mechanical Engineering, Hanyang University) ;
  • Lee, Jungsoo (Department of Mechanical Engineering, Hanyang University) ;
  • Kim, Donghwa (Department of Mechanical Engineering, Hanyang University) ;
  • Cho, Jinsoo (Department of Mechanical Engineering, Hanyang University)
  • Received : 2016.07.25
  • Accepted : 2016.10.20
  • Published : 2017.02.01

Abstract

Optimization process of pre-swirl nozzle geometry was conducted to improve the discharge coefficient of pre-swirl system by using CFD. The optimization of pre-swirl nozzle shape covered the converging angle and the location of the converging nozzle. Optimization process included Optimal Latin Hyper-cube Design method to get the experimental points and the Kriging method to create the response surface which gives candidate points. The process was finished when the difference between the predicted value and CFD value of candidate point was less than 0.1 %. This paper compared the Reference model, Initial model which is the first model of optimization and Optimized model to study flow characteristics. Finally, the discharge coefficient of Optimized model is improved about 17 % to the Reference model.

Keywords

References

  1. Dittmann, M., Geis, T., Schramm, V., Kim, S., and Wittig, S., 2002, "Discharge Coefficients of a Preswirl System in Secondary Air Systems," ASME Journal of Turbomachinery, Vol. 124, pp. 119-124. https://doi.org/10.1115/1.1413474
  2. Javiya, U., Chew, J., and Hills, N., 2011, "A Comparative Study of Cascade Vanes and Drilled Nozzle Designs for Pre-Swirl," ASME Turbo Expo, Vancouver, British Columbia, Canada, GT-2011-4006.
  3. Lewis, P., Wilson, M., Lock, G., and Owen, J. M., 2008, "Effect of Radial Location of Nozzles on Performance of Pre-Swirl Systems," ASME Turbo Expo, Berlin, Germany, GT-2008-50295.
  4. Bricaud, C., Geis, T., Dullenkopf, K., and Bauer, H. J., 2007, "Measurement and Analysis of Aerodynamic and Thermodynamic Losses in Pre-Swirl System Arrangements," ASME Turbo Expo, Montreal, Canada, GT-2007-27191.
  5. Chew, J. W., Ciampoli, F., Hills, N. J., and Scanlon, T., 2005, "Pre-Swirled Cooling Air Delivery System Performance," ASME Turbo Expo, Reno-Tahoe, Nevada, USA, GT-2005-68323.
  6. Ciampoli, F., Chew, F. W., Shahpar, S., and Willocq, E., 2006, "Automatic Optimisation of Pre-Swirl Nozzle Design," ASME Turbo Expo, Barcelona, Spain, GT- 2006-90249.
  7. Lewis, P., 2008, "Pre-swirl rotor-stator systems: Flow and heat transfer," PH. D. Thesis, Department of Mechanical Engineering, University of Bath.
  8. Yan, Y., Gord, M. F., Lock, G. D., Wilson, M., and Owen, F. M., 2003, "Fluid Dynamics of a Pre-Swirl Rotor-Stator System," ASME Journal of Turbomachinery, Vol. 125, pp. 641-647. https://doi.org/10.1115/1.1578502
  9. Simpson, T., Mauery, T. M., Korte, J. J., and Mistree, F., 2001, "Kriging Models for Global Approximation in Simulation-based Multidisciplinary Design Optimization," AIAA Journal, Vol. 39, No. 12, pp. 2233-2241. https://doi.org/10.2514/2.1234
  10. Seong, S., Murayama, M., and Yamamoto, K., 2005, "Efficient optimization design method using Kriging model," Journal of Aircraft, vol. 42, No. 2, pp. 413-420. https://doi.org/10.2514/1.6386
  11. Ahmed, M. Y. M. and Qin, N., 2009, "Comparison of Response Surface and Kriging Surrogates in Aerodynamic Design Optimization of Hypersonic Spiked Blunt Bodies," ASAT-13.
  12. Myers, R. H. and Montgomery, D. C., 2001, "Response Surface Methodology," Wiley Interscience Publication.
  13. Cagan, M., Benim, A. C., and Gunes, D., 2009, "Computational Analysis of Gas Turbine Preswirl System Operation Characteristics," WSEAS TRANSACTIONS on FLUID MECHANICS, Issue 4, Vol. 4, pp. 117-126.
  14. Feng, Z., Xinjun, W., Gaoliang, L., and Jun, L., 2015, "Computational fluid dynamics analysis for effect of length to diameter ratio of nozzles on performance of pre-swirl systems," Journal of POWER AND ENERGY, Vol. 229, No. 4, pp. 381-392. https://doi.org/10.1177/0957650915582352
  15. Benim, A. C., Cagan, M., Bonhoff, B., and Brillert, D., 2005, "Simulation of flow in Gas Turbine Pre-Swirl Systems with Emphasis on Rotor-Stator Interface Treatment," WSEAS int. Conf. on FLUID DYNAMICS & AERODYNAMICS, Corfu, Greece, pp. 206-211, August 20-22.

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