The Ultrahigh Efficiency Gas Turbine Engine With Stator Internal Combustion
暂无分享,去创建一个
[1] T. O’Doherty,et al. Vortex breakdown: a review , 2001 .
[2] N. Syred,et al. The effect of swirl burner aerodynamics on NOx formation , 1981 .
[3] Thomas Sattelmayer,et al. Double-Cone Burners for Gas Turbine Type 9 Retrofit Application , 1991 .
[4] W. Egli,et al. Vortex breakdown as a fundamental element of vortex dynamics , 1988 .
[5] Je-Chin Han,et al. A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness Under Rotation Condition , 2015 .
[6] A. Lefebvre. Gas Turbine Combustion , 1983 .
[7] Achmed Schulz,et al. Impact of Swirl Flow on the Cooling Performance of an Effusion Cooled Combustor Liner , 2012 .
[8] F. Lacas,et al. Mixing and stabilization study of a partially premixed swirling flame using laser induced fluorescence , 2011 .
[9] Meinhard T. Schobeiri,et al. A Comparative Numerical Study of Aerodynamics and Heat Transfer on Transitional Flow Around a Highly Loaded Turbine Blade With Flow Separation Using RANS, URANS and LES , 2014 .
[10] Alan H. Epstein,et al. Analysis of Hot Streak Effects on Turbine Rotor Heat Load , 1997 .
[11] M. Heitor,et al. Swirl flow structure and flame characteristics in a model lean premixed combustor , 2003 .
[12] Thomas Povey,et al. Effect of Simulated Combustor Temperature Nonuniformity on HP Vane and End Wall Heat Transfer: An Experimental and Computational Investigation , 2011 .
[13] Karen A. Thole,et al. Effects of Combustor Exit Profiles on Vane Aerodynamic Loading and Heat Transfer in a High Pressure Turbine , 2009 .
[14] Meinhard T. Schobeiri,et al. Experimental Study of the Effect of Periodic Unsteady Wake Flow on Boundary Layer Development, Separation, and Reattachment Along the Surface of a Low Pressure Turbine Blade , 2004 .
[15] Paul F. Beard,et al. Effect of Combustor Swirl on Transonic High Pressure Turbine Efficiency , 2014 .
[16] Reza S. Abhari,et al. Effect of Hot Streak Migration on Unsteady Blade Row Interaction in an Axial Turbine , 2010 .
[17] P. Adami,et al. Analysis of Radial Migration of Hot-Streak in Swirling Flow Through High-Pressure Turbine Stage , 2013 .
[18] Meinhard T. Schobeiri,et al. Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model , 2002 .
[19] Meinhard T. Schobeiri,et al. An Experimental and Numerical Study of the Effects of Flow Incidence Angles on the Performance of a Stator Blade Cascade of a High Pressure Steam Turbine , 2009 .
[20] Meinhard T. Schobeiri,et al. Effect of unsteady wake passing frequency on boundary layer transition, experimental investigation and wavelet analysis , 1995 .
[21] Randall M. Mathison,et al. Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine: Part I—Vane Inlet Temperature Profile Generation and Migration , 2010 .
[22] Thomas Povey,et al. Analysis on the Effect of a Nonuniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine Stages , 2012 .
[23] Sébastien Ducruix,et al. Studying the Stabilization Dynamics of Swirling Partially Premixed Flames by Proper Orthogonal Decomposition , 2012 .
[24] Meinhard T. Schobeiri. Turbomachinery Flow Physics and Dynamic Performance , 2004 .
[25] Arthur H. Lefebvre,et al. The Role of Fuel Preparation in Low-Emission Combustion , 1995 .
[26] David G. Lilley,et al. Swirl Flows in Combustion: A Review , 1977 .
[27] Achmed Schulz,et al. A New Test Facility for Investigating the Interaction Between Swirl Flow and Wall Cooling Films in Combustors , 2009 .
[28] L. Wright,et al. The Effect of Periodic Unsteady Flow on Aerodynamics and Heat Transfer on a Curved Surface , 1999 .
[29] R. Koch,et al. Effects of Pilot Fuel and Liner Cooling on the Flame Structure in a Full Scale Swirl-Stabilized Combustion Setup , 2010 .