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Gas Turbine Heat Transfer

Table of Contents:

UNSTEAD 3-D HEAT TRANSFER COMPUTATIONS IN ROTOR BLADE PASSAGES
Ryo S. Amano, B. Lin
pages 475-480
$25.00
DESIGN OF SYSTEM OF COOLING OF NOZZLE VANE OF GASTURBINE FOR DRIVING GTI
K. D. Andreev, L.V. Arseniev, V. G. Polishchuk, N. P. Sokolov, S.M. Vokchmyanin , U.A. Rusetskiy
pages 481-490
$25.00
ANALYSES OF LIQUID AND VAPOR FLOW IN A MINIATURE RADIALLY ROTATING HEAT PIPE FOR TURBINE BLADE COOLING APPLICATIONS
Yiding Cao, Jian Ling, Won Soon Chang
pages 491-497
$25.00
EFFECTS OF HOLE GEOMETRY ON HEAT (MASS) TRANSFER AND FILM COOLING EFFECTIVENESS
Hyung-Hee Cho, Byunggu Kim, Dong Ho Rhee
pages 499-504
$25.00
Heat Transfer of Film Cooling on a Radially Rotating Cylinder
G. J. Hwang, Y. J. Cheng
pages 505-510
$25.00
HEAT TRANSFER ON NON-POROUS AND POROUS SMOOTH END WALLS OF A LINEAR GUIDE VANE MODEL
Artem Khalatov
pages 511-516
$25.00
INVESTIGATIONS OF THE EFFECTS OF BULK FLOW PULSATIONS ON FILM COOLING AS APPLIED TO GAS TURBINE ENGINES
Phillip Ligrani, Joon Sik Lee, H. J. Seo
pages 517-522
$25.00
THERMOFLUID BEHAVIOR IN THE CAVERN FORTHE COMPRESSED AIR ENERGY STORAGE GAS TURBINE SYSTEM
Hideo Yoshida, Sigeru Tada, Yasushi Oishi , Takahiro Hatoya, Ryozo Echigo, Cho - Young Hang
pages 523-528
$25.00
CONVECTIVE HEAT TRANSFER COEFFICIENT ON A MULTIHOLED PLATE REPRESENTATIVE OF A COMBUSTION CHAMBER WALL
J.M Emidio, G. Grienche , G. Schott, B. Leger, P. Andre
pages 529-534
$25.00
THE METHOD OPTIMIZATION OF GAS TURBINE BLADES COOLING SYSTEM
Boris M. Galitseisky, A. V. Loburev , M. S. Cherny
pages 535-540
$25.00
A NUMERICAL STUDY ON A SUPERSONIC COMPRESSOR CASCADE USING R-ε TURBULENCE CLOSURE
S. D. Kim, I. K. Chung , D. J. Song
pages 541-546
$25.00
THERMAL STRATIFICATION AND FLOW STABILITY IN FILM COOLING WITH CURVED COOLANT INJECTION
Geun Sik Lee, Wen-Jei Yang, Chuan-Hsien Kuo
pages 547-552
$25.00
UNSTEADY LAMINAR FLOW AND HEAT TRANSFER IN A ROTATING CAVITY WITH A STATIONARY OUTER SURFACE
T. W. Lewis, M. Wilson , D. Andrew S. Rees
pages 553-557
$25.00
HEAT TRANSFER ENHANCEMENT IN A CIRCULAR CHANNEL USING LENGTHWISE CONTINUOUS TANGENTIAL INJECTION
Hee-Koo Moon, T. O'Connell , B. Glezer
pages 559-564
$25.00
LARGE EDDY SIMULATION APPLIED TO INTERNAL FORCED-CONVECTION COOLING OF GAS-TURBINE BLADES
Akira Murata, Sadanari Mochizuki
pages 565-570
$25.00
FILM TEMPERATURE AND EFFECTIVENESS MEASUREMENTS ON A CYLINDRICAL LEADING EDGE FILM COOLING MODEL
Dong Kee Sohn, Shuye Teng, Je-Chin Han
pages 571-576
$25.00
EFFECT OF ENDWALL BOUNDARY CONDITIONS ON TURBINE BLADE MASS TRANSFER IN THE PRESENCE OF HIGH FREESTREAM TURBULENCE
Hai-Ping Wang , Richard J. Goldstein
pages 577-582
$25.00