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会议文集


文集名Heat Transfer - Combustors; Film Cooling
会议名2022 ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT 2022)
中译名《2022年ASME涡轮机博览会：涡轮机技术会议与展览会，卷6A》
机构American Society of Mechanical Engineers (ASME)
会议日期13-17 June 2022
会议地点Rotterdam, Netherlands
出版年2022
馆藏号345403


题名作者出版年
ASSESSMENT OF A CONJUGATE HEAT TRANSFER METHOD ON AN EFFUSION COOLED COMBUSTOR OPERATED WITH A SWIRL STABILIZED PARTIALLY PREMIXED FLAMEA. Amerini; S. Paccati; L. Mazzei; A. Andreini2022
EXPERIMENTAL AND NUMERICAL STUDY ON EFFUSION COOLING CONFIGURATION FOR THE SWIRL CMC COMBUSTOR PLATFORMKun DU; Qihao CHEN; Tingrui LIANG; Yihao JIA; Cunliang LIU2022
EFFUSION COOLING: INFLUENCE OF PRESSURE DROPMichael Bonds; Nagaraja Rudrapatna; Benjamin H. Wahls; Rudy Dudebout; Srinath V. Ekkad; Ryan Meyer2022
NUMERICAL PREDICTION OF HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS ON A NOZZLE GUIDE VANE WITH REPRESENTATIVE COMBUSTOR OUTFLOWS. G. Tomasello; A. Andreini; T. Bacci; B. Facchini; S. Cubeda; L. Andrei2022
NUMERICAL STUDY OF COMBUSTOR-TURBINE INTERACTION BY USING HYBRID RANS-LES APPROACHS. G. Tomasello; A. Andreini; R. Meloni; S. Cubeda; L. Andrei; V. Michelassi2022
TURBINE VANE PASSAGE EXPERIMENTS DOCUMENTING EVOLUTION OF SECONDARY FLOWS WITH CHANGES IN COMBUSTOR COOLANT INJECTION FLOWRATESKedar P. Nawathe; Yong W. Kim; Terrence W. Simon2022
THE COOLING EFFECT OF COMBUSTOR EXIT LOUVER SCHEME ON A TRANSONIC NOZZLE GUIDE VANE ENDWALLShuo Mao; Kaiyuan Zhang; Daniel Van Hout; Wing F. Ng; Hongzhou Xu; Michael Fox2022
EXPERIMENTAL INVESTIGATION OF FLAME-FILM COOLING INTERACTIONS WITH AN ACADEMIC TEST RIG AND OPTICAL LASER DIAGNOSTICSSylvain Petit; Benjamin Quevreux; Romain Morin; Romain Guillot; Frederic Grisch; Pradip Xavier2022
EXPERIMENTAL STUDY OF FILM COOLING WITH FAVORABLE AND ADVERSE PRESSURE GRADIENTSRalph J. Volino; Matthew C. Gillcrist2022
FILM COOLING HOLE SHAPE EFFECTS ON TURBINE BLADE HEAT TRANSFER-PART I: COMPUTATIONAL COMPARISON TO EXPERIMENTSpencer Sperling; Hakan Aksoy; Louis Christensen; Jong Liu; Randall Mathison; Jeremy Nickol2022
FILM COOLING HOLE SHAPE EFFECTS ON TURBINE BLADE HEAT TRANSFER-PART II: EFFECTS OF MASS FLOW RATE AND UNSTEADINESSSpencer Sperling; Hakan Aksoy; Louis Christensen; Jong Liu; Randall Mathison; Jeremy Nickol2022
EXPERIMENTAL EVALUATION OF A WAVY TRAILING EDGE COOLING DESIGN AS AN ALTERNATIVE TO PRESSURE SIDE CUTBACK COOLINGIzhar Ullah; Timothy A. Burdett; Lesley M. Wright; Je-Chin Han; Ching-Pang Lee2022
OPTIMIZED FILM COOLING FLOW ON A CONTOURED ENDWALL WITHIN A TRANSONIC ANNULAR CASCADETimothy A. Burdett; Izhar Ullah; Lesley M. Wright; Je-Chin Han; John W. McClintic; Daniel C. Crites; Ardeshir Riahi2022
IDENTIFICATION OF FLUCTUATION MODES FOR A CYLINDRICAL FILM COOLING HOLE USING THE SPECTRAL PROPER ORTHOGONAL DECOMPOSITION METHODNicola Rosafio; Giove De Cosmo; Simone Salvadori; Mauro Carnevale; Daniela Anna Misul2022
LARGE EDDY SIMULATION BASED OPTIMIZATION OF A FAN-SHAPED COOLING HOLE GEOMETRY TO ENHANCE COOLING PERFORMANCEShubham Agarwal; Laurent Gicquel; Florent Duchaine; Nicolas Odier; Jerome Dombard; Damien Bonneau; Michel Slusarz2022
TURBINE VANE PASSAGE COOLING EXPERIMENTS WITH A CLOSE-COUPLED COMBUSTOR-TURBINE INTERFACE GEOMETRY PART 1: DESCRIBING THE FLOWKedar P. Nawathe; Aaditya R. Nath; Yong W. Kim; Terrence W. Simon2022
INFLUENCE OF POROSITY ON DOUBLE-WALLED EFFUSION-COOLED SYSTEMS FOR GAS TURBINE BLADESMatthew Courtis; Peter Ireland2022
EFFICIENT MODELLING OF BLADE FILM COOLING IN GAS TURBINESJustin Penrose; Laith Zori; David Pons; Juan Carlos Morales; Samir Rida; Sunil Patil2022
CONJUGATE HEAT TRANSFER OF CYLINDRICAL AND TRENCHED FILM COOLING DESIGNS WITH ARRAY JET IMPINGEMENTLukas Fischer; Andres Sanchez; Fabian Schleich; Fabian Feller; Richard Raffelt; Michael Pfitzner2022
HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS ON A FILM-COOLED PRESSURE SIDE: RESULTS AND ASSESSMENT OF THE IR-BASED MEASUREMENT TECHNIQUE RELIABILITYT. Bacci; A. Picchi; S. Galeotti; B. Facchini; S. Cubeda2022
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