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형상 및 경사 각도에 따른 난류 충돌 제트에 의한 과도 액정 기법을 이용한 열전달 특성에 대한 연구

A Study on Heat Transfer According to Inclined Angle and Surface Performance Using Turbulent Impingement Jet with a Liquid Crystal Transient Method

  • 임경빈 (한밭대학교 기계공학과) ;
  • 이창희 (한양대학교 기계공학과) ;
  • 이상훈 (한밭대학교 대학원 기계공학과)
  • 발행 : 2006.12.01

초록

Measurements of the local heat transfer coefficients on hemispherical convex and concave surfaces with a turbulent impinging jet were made. The Reynolds number used was 11000, 23000, 50000 and the nozzle- to- surface distance was L/d=2, 4, 6, 8, and 10 and the jet angle was a = $0^{\circ}$, $15^{\circ}$, $30^{\circ}$ and $40^{\circ}$. In case of concave surface, the Nusselt number at the stagnation point decreases as the jet angle increases and has the maximum value for L/d=6. The X-axis Nusselt number distributions exhibit secondary maxima at $0^{\circ}$ $\leq$ a $\leq$ $15^{\circ}$, L/d $\leq$ 4 for X/d<0(upstream) and at $0^{\circ}$ $\leq$ a $\leq$ $40^{\circ}$, L/d $\leq$ 4 and at $30^{\circ}$ $\leq$ a $\leq$ $40^{\circ}$, 4 < L/d $\leq$ 6 for X/d<0(downstream). The secondary maximum occurs at long distance from the stagnation point as the jet angle increases or the nozzle-to-surface distance decreases. In case of convex, correlations of the stagnation point Nusselt number according to Reynolds number, jet-to-surface distance ratio and dimensionless surface angle are presented. In the stagnation point, in term of Ren, n ranges from 0.43 in case of 2 $\leq$ L/d $\leq$ 6 to 0.45 in case of 6 < L/d $\leq$ 10, there agrees roughly appears to be laminar boundary layer result. The maximum Nusselt number, in this experiment, occurred in the direction of upstream. The displacement of the maximum Nusselt number from the stagnation point increases with increasing surface angle or decreasing nozzle-to-surface distance. On this condition about surface curvature D/d=10, the maximum displacement is about 0.7 times of the jet nozzle diameter. The ratio of the maximum Nusselt number to the stagnation Nusselt number increases as the jet angle increases.

키워드

참고문헌

  1. Baughn, J W., Hechanova, A. E. and Yan, X., 1991, 'An Experimental Study of Entrainment Effects on the Heat Transfer From a Flat Surface to a Heated Circular Impinging Jet,' ASME Joumal of Heat Transfer, Vol. 113, pp.1023-1025 https://doi.org/10.1115/1.2911197
  2. Baughn, J.W. and Yan, X., 1991b, 'A Preheated Wall Transient Method for Measurements of the Heat Transfer from a Surface to an Impinging Jet,' Proceedings, Eurothern Seminar, No. 25, Pau, France, pp. 1-7
  3. Gardon, R. and Akfirat, J.C., 1965, 'The Role of Turbulence in Determining the Heat Transfer Characteristics of Impinging Jets,' International Journal of Heat and Mass Transfer, Vol. 8, pp. 1261-1272 https://doi.org/10.1016/0017-9310(65)90054-2
  4. Gardon, R. and Cobonpue, J., 1962, 'Heat Transfer Between a Flat Plate and Jets of Air Impinging on It,' International Development in Heat Transfer, ASME, pp. 454-460
  5. Martin, H., 1977, 'Heat and Mass Transfer Between Impinging Gas Jet and Solid Surfaces,' Advances in Heat Transfer, Vol. 13, pp. 1-60 https://doi.org/10.1016/S0065-2717(08)70221-1
  6. Hrycak, P., Lee, D. T., Gauntner, J. W. and Livingood, J. N. B., 1970, 'Experimental Flow Characteristics of a Single Turbulent Jet Impinging on a Flat Plate,' NASA TN D-5690
  7. Lee, S.J., Lee, D. H. and Grief, R., 1993, 'Heat Transfer from a Plate to a Fully Developed Axsymmetric Impinging Jet,' Enhanced Cooling Techniques for Electronics Application, ASME HTD-Vol. 263, pp. 11-18
  8. Chupp, R.E., Helms, H.E., McFadden, P.W. and Brown, T.R., 1969, 'Evaluation of Internal Heat Transfer Coefficients for Impingement Cooled Turbine Airfoils,' J. of Aircraft, Vol. 6, No. 3, pp. 203-208 https://doi.org/10.2514/3.44036
  9. Thomann, H., 1968, 'Effect of Stream Wise Wall Curvature on Heat Transfer in a Turbulent Boundary Layer,' Journal of Fluid Mechanics, Vol. 33, pp. 282-292 https://doi.org/10.1017/S0022112068001308
  10. Hrycak, P., 1982, 'Heat Transfer and Flow Characteristics of Jets Impinging on a Concave Hemispherical Plate, ' Proceeding of International Heat Transfer Conference, pp. 357-362
  11. Goldstein, R, J. and Franchett, M.E., 1988, 'Heat Transfer from a Flat Surface to an Oblique Impinging Jet,' Journal of Heat Transfer, Vol. 110, pp. 84-90 https://doi.org/10.1115/1.3250477
  12. Gau, C. and Chung, C.M., 1991, 'Surface Curvature Effect on Slot-Air Jet Impinging Cooling Flow and Heat Transfer Process,' ASME Journal of Heat Transfer, Vol. 113, pp. 858-864 https://doi.org/10.1115/1.2911214
  13. Hoogendoorn, C.J., 1977, 'The Effect of Turbulence on Heat Transfer at Stagnation Point,' Int. J. Heat Mass Transfer, Vol. 20, pp. 1333-1338 https://doi.org/10.1016/0017-9310(77)90029-1
  14. Goldstein, R.J. and Franchett, M.E., 1988, 'Heat Transfer from a Flat Surface to an Oblique Impinging Jet,' ASME J. Heat Transfer, Vol. 110, pp. 84-90 https://doi.org/10.1115/1.3250477
  15. Yan, X., 1993, 'A Preheated-Wall Transient Method Using Liquid Crystals for the Measurement of Heat Transfer on External Surfaces and in Ducts,' Ph.D. Dissertation, University of California, Davis
  16. Lim, K.B., 1995, 'Measurement of the Heat Transfer Coefficient on a Concave Surface with a Turbulent Round Impinging Jet,' The Society of Airconditioning and Refrigerating Engineers of Korea, No. 1, pp. 112-119
  17. Lee, D.H., Chung, Y.S., Kim, D.S. and Lim, K.B., 1997, 'Heat Transfer and Flow Characteristics of a Circular Jet Impinging on a Convex Curved Surface,' Trans. of the KSME(B), Vol. 21, No. 4, pp. 579-588
  18. Baughn, J.W. and Yan, X., 1991a, 'An Insertion Technique Using the Transient Method with Liquid Crystals for Heat Transfer Measurements in Ducts,' Fouling and Enhancement Interactions, Rabas, T.J. and Chenoweth, J.M., Edited, ASME HTD-Vol. 164, pp 77-83
  19. Yan X., Baughn, J.W. and Mesbah, M., 1992, 'The Effect of Reynolds Number on the Heat Transfer Distribution from a Flat Plate to an Impinging Jet,' ASME HTD-Vol. 226, pp. 11-18
  20. Schlichting, H., 1979, Boundary Layer Theory, 7th ed., McGraw-Hill, New York
  21. Vedula, R.P., Metzger, D.E. and Bickford, W.B., 1988, 'Effect of Lateral and Anisotropy Conduction on Determination of Local Convection Heat Transfer Characteristics with Transient Tests and Surface Coating,' ASME Collected Papers in Heat Transfer, HTD-Vol. 104, pp. 21-27
  22. Kline, S.J. and Mcklintock, F.A., 1953, 'Describing Uncertainties in Single Sample Experiments,' Mechanical 'Engineering, Vol. 75, No. 1, pp. 3-8
  23. Yoon, S.H., Kim, M.K. and Lee, D.H., 1996, 'Turbulence Flow and Heat Transfer Characteristics of a Two-Dimensional Oblique Plate Impinging Jet,' KSME Int. J., Vol. 11, No. 4, pp. 476-483
  24. Chan, T.L., Ashfort-Frost, S. and Jambunathan, K., 2001, 'Calibrating for Viewing Angle Effect During Heat Transfer Measurements on a Curved Surface,' Int. J. of heat and mass transfer, 44, pp. 2209-2223 https://doi.org/10.1016/S0017-9310(00)00267-2