An investigation of the heat transfer and static pressure on the over-tip casing wall of an axial turbine operating at engine representative flow conditions. (II). Time-resolved results
暂无分享,去创建一个
Roger W. Ainsworth | Neil William Harvey | Steven J. Thorpe | Shin Yoshino | S. Thorpe | R. Ainsworth | N. Harvey | Shin Yoshino
[1] T. V. Jones,et al. Heat-transfer measurements in short-duration hypersonic facilities , 1973 .
[2] H. Schlichting. Boundary Layer Theory , 1955 .
[3] Roger W. Ainsworth,et al. Unsteady Pressure Measurement , 2000 .
[4] Tony Arts,et al. Aero-Thermal Performance of a Two-Dimensional Highly Loaded Transonic Turbine Nozzle Guide Vane: A Test Case for Inviscid and Viscous Flow Computations , 1992 .
[5] Anthony G. Sheard,et al. A Transient Flow Facility for the Study of the Thermofluid-Dynamics of a Full Stage Turbine Under Engine Representative Conditions , 1988 .
[6] W. G. Steele,et al. Engineering application of experimental uncertainty analysis , 1995 .
[7] Richard J Goldstein,et al. Effects of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From a Large-Scale Gas Turbine Blade , 2003 .
[8] F. Martelli,et al. Investigation of the Unsteady Rotor Aerodynamics in a Transonic Turbine Stage , 2001 .
[9] J. P. Bindon,et al. The Effect of Tip Clearance on the Development of Loss Behind a Rotor and a Subsequent Nozzle , 1997 .
[10] Neil William Harvey,et al. Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part I: Vane-Rotor and Rotor-Vane Interaction , 2003 .
[11] Howard P. Hodson,et al. The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades , 1991 .
[12] D. E. Metzger,et al. Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models , 1995 .
[13] Richard J Goldstein,et al. Effect of Endwall Motion on Blade Tip Heat Transfer , 2003 .
[14] J. P. Bindon,et al. The measurement and formation of tip clearance loss , 1989 .
[15] D. E. Metzger,et al. The Influence of Turbine Clearance Gap Leakage on Passage Velocity and Heat Transfer Near Blade Tips: Part II—Source Flow Effects on Blade Suction Sides , 1989 .
[16] A. Yamamoto,et al. Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance , 1989 .
[17] Alan H. Epstein,et al. TIME RESOLVED MEASUREi.lENTS OF A TURBINE IROTUR STATIONARY TIP CASING PRESSURE AND HEAT Tt?AN!IFER FIELD , 1985 .
[18] Roger W. Ainsworth,et al. Heat Transfer to Rotating Turbine Blades in a Flow Undisturbed by Wakes , 1994 .
[19] J. G. Moore,et al. Flow and Heat Transfer in Turbine Tip Gaps , 1989 .
[20] A. J. Dietz,et al. Unsteady Pressure Measurements on the Rotor of a Model Turbine Stage in a Transient Flow Facility , 1992 .
[21] Gary D. Lock,et al. Endwall heat transfer measurements in an annular cascade of nozzle guide vanes at engine representative Reynolds and Mach numbers , 1996 .
[22] Michael G. Dunn,et al. Turbine Tip and Shroud Heat Transfer , 1991 .
[23] Roger W. Ainsworth,et al. Developments in Instrumentation and Processing for Transient Heat Transfer Measurement in a Full-Stage Model Turbine , 1989 .
[24] R S Bunker,et al. A Review of Turbine Blade Tip Heat Transfer , 2001, Annals of the New York Academy of Sciences.
[25] G. W. Meetham. Use of protective coatings in aero gas turbine engines , 1986 .