Dependence of Film Cooling Effectiveness on Three-Dimensional Printed Cooling Holes
暂无分享,去创建一个
[1] David G. Bogard,et al. Effects of Surface Roughness on Film Cooling , 1996 .
[2] David G. Bogard,et al. Rough Surface Effects on Film Cooling of the Suction Side Surface of a Turbine Vane , 2003 .
[3] Ho-Chan Kim,et al. Surface roughness prediction using measured data and interpolation in layered manufacturing , 2009 .
[4] D. Silva,et al. Dimensional error of selective laser sintering, three-dimensional printing and PolyJet models in the reproduction of mandibular anatomy. , 2009, Journal of cranio-maxillo-facial surgery : official publication of the European Association for Cranio-Maxillo-Facial Surgery.
[5] Diego Mendoza,et al. An analysis of CCD camera noise and its effect on pressure sensitive paint instrumentation system signal-to-noise ratio , 1997, ICIASF'97 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.
[6] David G. Bogard,et al. Degradation of film cooling performance on a turbine vane suction side due to surface roughness , 2006 .
[7] Richard J Goldstein,et al. Effect of Surface Roughness on Film Cooling Performance , 1984 .
[8] Pablo Irarrazaval,et al. Sensitivity analysis of geometric errors in additive manufacturing medical models. , 2015, Medical engineering & physics.
[9] Liu Tianshu,et al. Accuracy of Pressure-Sensitive Paint , 2001 .
[10] Gi Dae Kim,et al. A benchmark study on rapid prototyping processes and machines: Quantitative comparisons of mechanical properties, accuracy, roughness, speed, and material cost , 2008 .
[11] T. V. Jones. Theory for the use of foreign gas in simulating film cooling , 1999 .
[12] Richard J Goldstein,et al. Mass Transfer in the Neighborhood of Jets Entering a Crossflow , 1982 .
[13] Srinath V. Ekkad,et al. Gas Turbine Heat Transfer and Cooling Technology , 2012 .
[14] E. R. G. Eckert,et al. Film cooling following injection through inclined circular tubes , 1974 .
[15] D. Banerjee,et al. Mass "Heat… Transfer Downstream of Blockages With Round and Elongated Holes in a Rectangular Channel , 2007 .
[16] Achmed Schulz,et al. Discharge Coefficient Measurements of Film-Cooling Holes With Expanded Exits , 1998 .
[17] Achmed Schulz,et al. High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling , 2001 .
[18] Akhilesh P. Rallabandi,et al. TURBINE BLADE FILM COOLING USING PSP TECHNIQUE , 2010 .
[19] Robert P. Schroeder,et al. ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE , 2014, Journal of Turbomachinery.
[20] Karen A. Thole,et al. Gas Turbine Film Cooling , 2006 .
[21] S. C. Lau,et al. Effect of Trailing-Edge Ejection on Local Heat (Mass) Transfer in Pin Fin Cooling Channels in Turbine Blades , 1992 .
[22] Tianshu Liu,et al. Accuracy of pressure sensitive paint , 1999 .
[23] Robert J. Moffat,et al. Describing the Uncertainties in Experimental Results , 1988 .
[24] Je-Chin Han,et al. Influence of Coolant Density on Turbine Blade Platform Film-Cooling , 2009 .
[25] Je-Chin Han,et al. Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes , 1988 .
[26] Ronald Scott Bunker,et al. A review of shaped hole turbine film-cooling technology , 2005 .
[27] Robert P. Schroeder,et al. Effect of In-Hole Roughness on Film Cooling from a Shaped Hole , 2016 .
[28] S. Arunachalam,et al. Critical parameters influencing the quality of prototypes in fused deposition modelling , 2001 .