Handbook of Turbomachinery Second Edition Revised - Ventech!

89. R. P. Dring, M. F. Blair and H. D. Joslyn, ‘‘An Experimental Investigation of
Film Cooling on a Turbine Rotor Blade,’’ ASME J. Engineering for Power,
102: 81–87 (1980).
90. K. Takeishi, S. Aoki, T. Sato and K. Tsukagoshi, ‘‘Film Cooling on a Gas
Turbine Rotor Blade,’’ ASME Paper 91-GT-279 (1991).
91. R. S. Abhari and A. H. Epstein, ‘‘An Experimental Study of Film Cooling in a
Rotating Transonic Turbine,’’ ASME Paper 92-GT-187 (1992).
92. O. Uzo and C. Camci, ‘‘Aerodynamic Loss Characteristics of a Turbine Blade
with Trailing Edge Coolant Ejection Part 2, External Aerodynamics, Total
Pressure Losses and Predictions,’’ ASME Paper 2000-GT-258 (2000).
93. A. A. Ameri and R. S. Bunker, ‘‘Heat Transfer and Flow on the First Stage
Blade Tip of a Power Generation Gas Turbine Part 2; Simulation Results,’’
ASME Paper 99-GT-283 (1999).
94. J. P. Bindon, ‘‘Pressure and Flowfield Measurements of Axial Turbine Tip
Clearance Flow in a Linear Cascade,’’ Cambridge University Engineering
Department, TR 123 (1986).
95. R. S. Bunker and J. C. Bailey, ‘‘Effect of Squealer Cavity Depth and
Oxidation on Turbine Blade Tip Heat Transfer,’’ ASME Paper 2000-GT-
0155D (2000).
96. D. Dey and C. Camci, ‘‘Aerodynamic Tip Desensitization of an Axial Turbine
Rotor Using Tip Platform Extension,’’ ASME Paper 2001-GT-484 (2001).
97. N. W. Harvey and K. Ramsden, ‘‘A Computational Study of a Novel Turbine
Partial Shroud,’’ ASME Paper 2000-GT-668 (2000).
98. R. S. Bunker, ‘‘Review of Turbine Blade Tip Heat Transfer,’’ Turbine 2000
Symposium on Heat Transfer in Gas Turbine Systems, Cesme, Turkey (2000).
99. NASA Report, ‘‘Liquid Rocket Engine Turbopump Rotating Shaft Seals,’’
SP-8121 (1978).
100. J. G. Ferguson, ‘‘Brushes as High Performance Gas Turbine Seals,’’ ASME
Paper 88-GT-182 (1988).
101. B. Meierhofer and C. J. Franklin, ‘‘An Investigation of a Preswirled Cooling
Airflow to a Gas Turbine Disc by Measuring the Air Temperature in the
Rotating Channels,’’ ASME Paper 81-GT-132 (1981).
102. M. Wilson, R. Pilbrow and J. M. Owen, ‘‘Flow and Heat Transfer in a
Preswirl Rotor–Stator System,’’ ASME J. Turbomachinery, 119: 364–373
(1997).
103. Z. El-Oun and J. M. Owen, ‘‘Pre-Swirl Blade Cooling Effectiveness in an
Adiabatic Rotor–Stator System,’’ ASME J. Turbomachinery, 111: 522–529
(1989).
104. D. E. Metzger, W. J. Mathis and L. D. Grochowsky, ‘‘Jet Cooling at the Rim
of a Rotating Disc,’’ ASME Paper 78-GT-25 (1978).
105. R. P. Roy, G. Xu, J. Feng and S. Kang, ‘‘Pressure Field and Mainstream Gas
Ingestion in a Rotor–Stator Disk Cavity,’’ ASME Paper 2001-GT-0564
(2001).
Copyright © 2003 Marcel Dekker, Inc.