Combined Effects of Freestream Pressure Gradient and Density Ratio on the Film Cooling Effectiveness of Round and Shaped Holes on a Flat Plate
Tóm tắt
Từ khóa
Tài liệu tham khảo
2005, A Review of Shaped Hole Turbine Technology, ASME J. Heat Transfer, 127, 441, 10.1115/1.1860562
2012, Gas Turbine Heat Transfer and Cooling Technology, 2nd ed.
2001, High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling, ASME J. Turbomach., 123, 758, 10.1115/1.1371778
1974, Heat Transfer and Film Cooling Following Injection Through Inclined Circular Tubes, ASME J. Heat Transfer, 96, 239, 10.1115/1.3450171
2015, Film Cooling for Cylindrical and Fan-Shaped Holes Using Pressure-Sensitive Paint Measurement Technique, AIAA J. Thermophys. Heat Transfer, 29, 1, 10.2514/1.T4518
2011, Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP, ASME J. Turbomach., 133, 4, 10.1115/1.4002988
1996, Film Cooling With Compound Angle Holes: Adiabatic Effectiveness, ASME J. Turbomach., 118, 807, 10.1115/1.2840938
2014, An Experimental Study of Density Ratio Effects on the Film Cooling Injection From Discrete Holes by Using PIV and PSP Techniques, Int. J. Heat Mass Transfer, 76, 337, 10.1016/j.ijheatmasstransfer.2014.04.028
1991, Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio, ASME J. Turbomach., 113, 442, 10.1115/1.2927894
1977, Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy, ASME J. Heat Transfer, 99, 620, 10.1115/1.3450752
Thole, K. A., Sinha, A., Bogard, D. G., and Crawford, M. E., 1992, “Mean Temperature Measurements of Jets With a Crossflow for Gas Turbine Film Cooling Application,” 3rd International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3), Honolulu, HI, Apr. 1–4, pp. 69–85.
2001, An Experimental Investigation of Film Cooling on a Convex Surface Subjected to Favorable Pressure Gradient Flow, Int. J. Heat Mass Transfer, 44, 939, 10.1016/S0017-9310(00)00158-7
1991, Film Cooling in the Presence of Mainstream Pressure Gradients, ASME J. Turbomach., 113, 484, 10.1115/1.2927900
1975, Experimental Investigation of Film Cooling With Ejection From a Row of Holes for the Application to Gas Turbine Blades, ASME J. Eng. Gas Turbines Power, 97, 21, 10.1115/1.3445904
1974, Discrete-Hole Cooling in the Presence of Free Stream Turbulence and Strong Favorable Pressure Gradient, Int. J. Heat Mass Transfer, 17, 1403, 10.1016/0017-9310(74)90141-0
2012, Three-Dimensional Velocity Measurements of Film Cooling Flow Under Favorable Pressure Gradient, ASME, 10.1115/GT2012-69402
2005, Assessment of Steady State PSP, TSP, and IR Measurement Techniques for Flat Plate Film Cooling, ASME, 10.1115/HT2005-72363
2005, Assessment of Steady State PSP and Transient IR Measurement Techniques for Leading Edge Film Cooling, ASME, 10.1115/IMECE2005-80146
1953, Describing Uncertainties in Single-Sample Experiments, Mech. Eng., 75, 3