DOI QR코드

DOI QR Code

예인수조 LDV를 이용한 평판 경계층과 와이어 타입 난류촉진장치의 상호작용에 관한 연구

Towed Underwater LDV Measurement of the Interaction of a Wire-Type Stimulator and the Boundary Layer on a Flat Plate

  • 박종열 (서울대학교 조선해양공학과) ;
  • 서정화 (충남대학교 선박해양공학과) ;
  • 이신형 (서울대학교 조선해양공학과)
  • Park, Jongyeol (Department of Naval Architecture and Ocean Engineering, Seoul National University) ;
  • Seo, Jeonghwa (Department of Naval Architecture and Ocean Engineering, Chungnam National University) ;
  • Rhee, Shin Hyung (Department of Naval Architecture and Ocean Engineering, Seoul National University)
  • 투고 : 2021.03.11
  • 심사 : 2021.06.23
  • 발행 : 2021.08.20

초록

The present study aims to investigate the interaction of a wire-type turbulence stimulator and the laminar boundary layer on a flat plate by flow field measurement. For the towing tank tests, a one-dimensional Laser Doppler Velocimetry (LDV) attached on a two-axis traverse was used to measure the streamwise velocity component of the boundary layer flow in zero pressure gradient, disturbed by a turbulence stimulator. The wire diameter was 0.5 and 1.0 mm according to the recommended procedures and guidelines suggested by the International Towing Tank Conference. Turbulence development by the stimulator was identified by the skin friction coefficient, mean and Root Mean Square (RMS) of the streamwise velocity. The laminar boundary layer with the absence of the wire-type stimulator was similar to the Blasius solution and previous experimental results. By the stimulator, the mean and RMS of the streamwise velocity were increased near the wall, showing typical features of the fully developed turbulent boundary layer. The critical Reynolds number was reduced from 2.7×105 to 1.0×105 by the disturbances caused by the wire. As the wire diameter and the roughness Reynolds number (Rek) increased, the disturbances by the stimulator increased RMS of the streamwise velocity than turbulent boundary layer.

키워드

과제정보

본 연구는 한국연구재단(NRF-2020R1I1A2074369, NRF-2021R1A6A3A13045434)의 지원을 받아 수행되었으며, 서울대학교 공학연구원의 지원에도 감사를 드립니다.

참고문헌

  1. Clauser, F.H., 1956. The turbulent boundary layer. Advances in Applied Mechanics, 4, pp.1-51. https://doi.org/10.1016/S0065-2156(08)70370-3
  2. Dos Santos, F.L., Sanders, M.P.J., de Santana, L.D., & Venner, C.H., 2020. Influence of tripping devices in hastening transition in a flat plate submitted to zero and favorable pressure gradients. Proceedings of the AIAA Scitech 2020 Forum, Orlando, United States of America. 6-10 January 2020, 0046.
  3. Elsinga, G.E., & Westerweel, J., 2012. Tomographic-PIV measurement of the flow around a zigzag boundary layer trip. Experiments in Fluids, 52(4), pp.865-876. https://doi.org/10.1007/s00348-011-1153-8
  4. Fransson, J.H., Brandt, L., Talamelli, A., & Cossu, C., 2004. Experimental and theoretical investigation of the nonmodal growth of steady streaks in a flat plate boundary layer. Physics of Fluids, 16(10), pp.3627-3638. https://doi.org/10.1063/1.1773493
  5. Hanson, R.E., Buckley, H.P., & Lavoie, P., 2012. Aerodynamic optimization of the flat-plate leading edge for experimental studies of laminar and transitional boundary layers. Experiments in Fluids, 53(4), pp.863-871. https://doi.org/10.1007/s00348-012-1324-2
  6. Huber, A.F., & Mueller, T.J., 1987. The effect of trip wire roughness on the performance of the Wortmann FX 63-137 airfoil at low Reynolds numbers. Experiments in Fluids, 5(4), pp.263-272. https://doi.org/10.1007/BF00279740
  7. ITTC, 2002. Procedures for resistance, propulsion and propeller open water tests. 23rd International Towing Tank Conference, Venice, Italy. 8-14, September, 2002, 7.5-01-01-01.
  8. Jiang, X.Y. et al., 2020. Experimental study on low-speed streaks in a turbulent boundary layer at low Reynolds number. Journal of Fluid Mechanics, 903. https://doi.org/10.1017/jfm.2014.484
  9. Kendall, A., & Koochesfahani, M., 2008. A method for estimating wall friction in turbulent wall-bounded flows. Experiments in Fluids, 44(5), pp.773-780. https://doi.org/10.1007/s00348-007-0433-9
  10. Lee, S.B., 2018. Direct numerical and large eddy simulations of transitional flows around turbulence stimulators at very low speeds. Journal of the Society of Naval Architects of Korea, 55(3), pp.265-273. https://doi.org/10.3744/SNAK.2018.55.3.265
  11. Longo, J., Huang, H.P., & Stern, F., 1998. Solid/free-surface juncture boundary layer and wake. Experiments in Fluids, 25(4), pp.283-297. https://doi.org/10.1007/s003480050232
  12. Musker, A.J., 1979. Explicit expression for the smooth wall velocity distribution in a turbulent boundary layer. AIAA Journal, 17(6), pp.655-657. https://doi.org/10.2514/3.61193
  13. Paik, B.G. et al., 2013. Study on the drag performance of the flat plates treated by antifouling paints. Journal of the Society of Naval Architects of Korea, 50(6), pp.399-406. https://doi.org/10.3744/SNAK.2013.50.6.399
  14. Purtell, L.P., Klebanoff, P.S., & Buckley, F.T., 1981. Turbulent boundary layer at low Reynolds number. Physics of Fluids, 24(5), pp.802-811. https://doi.org/10.1063/1.863452
  15. Smith, A.M.O., & Clutter, D.W., 1959. The smallest height of roughness capable of affecting boundary-layer transition. Journal of the Aerospace Sciences, 26(4), pp.229-245. https://doi.org/10.2514/8.8019
  16. Spalart, P.R., 1988. Direct simulation of a turbulent boundary layer up to Rθ= 1410. Journal of Fluid Mechanics, 187, pp.61-98. https://doi.org/10.1017/S0022112088000345
  17. Spalding, D., 1961. A single formula for the "Law of the wall". Journal of Applied Mechanics, 455.
  18. Williams, O.J., Sahoo, D., Baumgartner, M.L., & Smits, A.J., 2018. Experiments on the structure and scaling of hypersonic turbulent boundary layers. Journal of Fluid Mechanics, 834, pp.237-270. https://doi.org/10.1017/jfm.2017.712
  19. Wu, X., & Moin, P., 2009. Direct numerical simulation of turbulence in a nominally zero-pressure-gradient flat-plate boundary layer. Journal of Fluid Mechanics, 630, pp.5-41. https://doi.org/10.1017/S0022112009006624