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풍력 블레이드의 결빙에 의한 공력 영향성 전산 예측

COMPUTATIONAL PREDICTION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF A WIND TURBINE BLADE

  • 박지호 (경상대학교 항공우주특성화대학원) ;
  • 정기영 (경상대학교 항공우주특성화대학원) ;
  • 명노신 (경상대학교 항공우주시스템공학과 및 항공기부품기술연구소)
  • Park, J.H. (Specialized Graduate School of Aerospace Engineering, Gyeongsang Nat'l Univ.) ;
  • Jung, K.Y. (Specialized Graduate School of Aerospace Engineering, Gyeongsang Nat'l Univ.) ;
  • Myong, R.S. (Dept. of Aerospace and System Engineering & Research Center for Aircraft Parts Technology, Gyeongsang Nat'l Univ.)
  • 투고 : 2013.07.11
  • 심사 : 2013.08.09
  • 발행 : 2013.09.30

초록

A significant change in aerodynamic characteristics of wind turbine blade can occur by ice formed on the surface of the blade operated in cold climate. The ice accretion can result in performance loss, overloading due to delayed stall, and excessive vibration associated with mass imbalance. In this study, the impact of ice accretion on the aerodynamic characteristics of NREL 5MW wind turbine blade sections is examined by a CFD-based method. It is shown that the thickness of ice accretion increases from the root to the tip and the effects of icing conditions such as relative wind velocity play a significant role in the shape of ice accretion. In addition, the computational results are used to assess the degradation in the lift and drag coefficients of the blade sections.

키워드

참고문헌

  1. 2012, Oh, M.W. and Kim, D.H., "Design and Computational Analysis of Small Vertical-Axis Wind Turbine for Ocean Buoy System," The Wind Engineering Institute of Korea, Vol.16, No.2, pp.49-45.
  2. 2012, Fernando, V., Marcelo, R. and Adrian, I., "Numerical Study of Flow Iced Wind Turbine Airfoil," Engineering Applications of Fluid Mechanics, Vol.6, No.1, pp.39-45. https://doi.org/10.1080/19942060.2012.11015401
  3. 2010, Muhammad, S.V., "Numerical Analysis of Atmospheric Ice Accretion on Wind Turbine Blades & Resultant Performance Losses," The Norwegian Research Council, Department of Technology, Narvik University College, Norway.
  4. 2000, Gent, R.W., Dart, N.P. and Cansdale, J.T., "Aircraft Icing," Phil. Trans. R. Soc. Lond, Vol.358, pp.2873-2911. https://doi.org/10.1098/rsta.2000.0689
  5. 1998, Kind, R.J., Potapczuk, M.G., Feo, A., Golia, C. and Shah, A.D., "Experimental and Computational Simulation of In-Flight Icing Phenomena," Progress in Aerospace Sciences, Vol.34, pp.257-345. https://doi.org/10.1016/S0376-0421(98)80001-8
  6. 2010, Jung, S.K., Myong, R.S. and Cho, T.H., "An Eulerian-Based Droplet Impingement and Ice Accretion Code for Aircraft Icing Prediction," Journal of Computational Fluids Engineering, Vol.15, No.2, pp.71-78.
  7. 2010, NTI Solutions User Manual, Newmerical Technologies Inc.
  8. 2002, Papadakis, M., Hung, K.E., Vu, G.T., Yeong, H.W., Bidwell, C.S., Breer, M.D. and Bencic, T.J., "Experimental Investigation of Water Droplet Impingement on Airfoils, Finite Wings, and an S-Duct Engine Inlet," NASA TM-2002-211700.
  9. 2011, Jung, S.K., Lee, C.H., Nagdewe, S., Myong, R.S. and Cho, T.H., "A Study on Truncated Flapped Airfoil for Efficient Icing Wind Tunnel Test," (in Korean) Journal of The Korean Society for Aeronautical and Space Sciences, Vol.39, No.6, pp.481-486. https://doi.org/10.5139/JKSAS.2011.39.6.481
  10. 2012, An, Y.G. and Myong, R.S., "Scaling Methods for Icing Wind Tunnel Test," (in Korean) Journal of The Korean Society for Aeronautical and Space Sciences, Vol.40, No.2, pp.1-8. https://doi.org/10.5139/JKSAS.2012.40.2.146
  11. 1997, Tezok, F. and Ernest, F., "Icing Tunnel Testing Methodology: Pre-Test CFD, Tunnel Peculiarities, Scaling Effects," Proc. of The Aerodynamics Symposium, Vol.6, pp.81-100.
  12. 2008, Kim, B.S., Kim, M.E. and Lee, Y.H., "Predicting the Aerodynamic Characteristics of 2D Airfoil and the Performance of 3D Wind Turbine using a CFD Code," Transactions of the KSME B, Vol.32, No.7, pp.549-557.
  13. 1997, Sommers, D.M., "Design and Experimental Results for the S809 Airfoil," NREL/SR-440-6918.
  14. 2011, Jung, S.K., Shin, S.M., Myong, R.S. and Cho, T.H., "An Efficient CFD-based Method for Aircraft Icing Simulation Using a Reduced Order Model," Journal of Mechanical Science and Technology, Vol.25, pp.703-711. https://doi.org/10.1007/s12206-011-0118-4
  15. 2009, Shin, H.B., Choi, W., Seo, S.J. and Ryu, J.B., "Study of Icing Accretion on The 2D Airfoil," (in Korean) Korean Society of Computational Fluid Engineering Spring Conference, pp.21-26.
  16. 2011, ANSYS V13.0 FLUENT Basic, TSNE.
  17. 2010, Jung, S.K., Shin, S.M., Myong, R.S., Cho, T.H., Jeong, H.H. and Jung, J.H., "Ice Accretion Effect on the Aerodynamic Characteristics of KC-100 Aircraft," 48th AIAA Aerospace Sciences Meeting, AIAA-2010-1237.
  18. 1999, Bourgault, Y., Habashi, W.G., Dompierre, J. and Baruzzi, G.S., "A Finite Element Method Study of Eulerian Droplets Impingement Models," International Journal for Numerical Methods in Fluids, Vol.4, pp.429-499.
  19. 2003, Beaugendre, H., Morency, F. and Habashi, W.G., "FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D," Journal of Aircraft, Vol.40, No.2, pp. 239-247. https://doi.org/10.2514/2.3113
  20. 2010, Lee, C.H., Shin, S.M., Jung, S.K., Myong, R.S., Cho, T.H., Jung, J.H. and Jeong, H.H., "Icing Effects on Aero -dynamic Characteristics of the Main Wing Section of KC-100 Aircraft," Proc. of the 2010 KSCFE Spring Conference, pp.323-362.
  21. 2003, Silveria, R.A., Malika, C.R., Estivam, D.A. and Mendes, R., "Evaluation of Collection Efficiency Methods for Icing Analysis," International Congress of Mechanical Engineering, COBEM2003-1810.

피인용 문헌

  1. Atmospheric Icing Effects on the Aerodynamic Characteristics and Performance of Wind Turbine Blade vol.42, pp.2, 2014, https://doi.org/10.5139/JKSAS.2014.42.2.134
  2. A Numerical Study on Icing Phenomenon of Wind Turbine Blade vol.20, pp.3, 2013, https://doi.org/10.17958/ksmt.20.3.201806.347
  3. 항공기 결빙 보호장치의 기술 현황 및 전망 vol.48, pp.11, 2013, https://doi.org/10.5139/jksas.2020.48.11.911