Affiliation:
1. Department of Mechanical Engineering, United States Naval Academy, Annapolis, Maryland 21402
Abstract
The effect of an unheated starting length upstream of a row of film cooling holes was studied experimentally to determine its effect on heat transfer coefficients downstream of the holes. Cases with a single row of cylindrical film cooling holes inclined at 35deg to the surface of a flat plate were considered at blowing ratios of 0.25, 0.5, 1.0, and 1.5. For each case, experiments were conducted to determine the film-cooling effectiveness and the Stanton number distributions in cases with the surface upstream of the holes heated and unheated. Measurements were made using an infrared camera, thermocouples, and hot and cold-wire anemometry. Ratios were computed of the Stanton number with film cooling (Stf) to corresponding Stanton numbers in cases without film cooling (Sto), but the same surface heating conditions. Contours of these ratios were qualitatively the same regardless of the upstream heating conditions, but the ratios were larger for the cases with a heating starting length. Differences were most pronounced just downstream of the holes and for the lower blowing rate cases. Even 12 diameters downstream of the holes, the Stanton number ratios were 10–15% higher with a heated starting length. At higher blowing rates the differences between the heated and unheated starting length cases were not significant. The differences in Stanton number distributions are related to jet flow structures, which vary with blowing rate.
Reference10 articles.
1. Film Cooling With Compound Angle Holes: Heat Transfer;Sen;ASME J. Turbomach.
2. Schmidt, D. L., and Bogard, D. G., 1996, “Effects of Free-Stream Turbulence and Surface Roughness on Film Cooling,” ASME Paper No. 96-GT-462.
3. Mayhew, J. E., Baughn, J. W., and Byerley, A. R., 2002, “The Effect of Freestream Turbulence on Film Cooling Heat Transfer Coefficient,” ASME Paper No. GT-2002-30173.
4. Kelly, G. B., and Bogard, D. G., 2003, “An Investigation of the Heat Transfer for Full Coverage Film Cooling,” ASME Paper No. GT2003-38716.
5. Burd, S., and Simon, T. W., 2000, “Effects of Hole Length, Supply Plenum Geometry, and Freestream Turbulence on Film Cooling Performance,” NASA CR-2000-210336.
Cited by
14 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献