ASME/TURBO 2000-2002三届年会采用FLUENT软件发表的论文

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ASME2002年
1  GT-2002-30090CFD-BASED, PARAMETRIC, DESIGN TOOL FOR GAS TURBINE COMBUSTORS FROM COMPRESSOR DESWIRL EXIT TO TURBINE INLETMark K. Lai, Robert S. Reynolds & Jeffrey ArmstrongCombustion & EmissionsEngines, Systems & Services, Honeywell International111 S 34 th Street, P.O. Box 52181Phoenix, AZ 85072-2181Email: Mark.Lai@Honeywell.com
2  GT-2002-30620DEVELOPMENT OF N (D PTIVE)UNSTRUCTURED 2-D INVERSE DESIGNMETHOD FOR TURBOM CHINERY BLADESBenjamin M.F.Choo and Mehrdad ZangenehDepartment of Mechanical Engineering,University College London,Torrington Place,London WC1E 7JE,United Kingdom.
3  GT-2002-30493AERODYNAMIC OPTIMISATION OF AN AEROENGINE BYPASS DUCT OGV-PYLON CONFIGURATIONThomas TschirnerRolls Royce Deutschland plc & Co KGEschenweg 11, D-15827 Dahlewitz, Germanyemail: thomas.tschirner@rolls-royce.comMichael PfitznerRolls Royce Deutschland plc & Co KGEschenweg 11, D-15827 Dahlewitz, Germanyemail: michael.pfitzner@unibw-muenchen.deRüdiger MerzRolls Royce Deutschland plc & Co KGEschenweg 11, D-15827 Dahlewitz, Germanyemail: ruediger.merz@rolls-royce.com
4  GT-2002-30246CALCULATION OF SURFACE ROUGHNESS EFFECTS ON AIR-RIDING SEALSC. GuardinoFluids Research Center,School of Engineering,University of Surrey,Guildford, Surrey GU2 7XH, UKJ. W. ChewFluids Research Center,School of Engineering,University of Surrey,Guildford, Surrey GU2 7XH, UKN. J. HillsThermo-Fluid Mechanics Research Centre, School of Engineering and Information Technology,University of Sussex, Falmer, Brighton BN1 9QT UK
5  GT-2002-30525EFFECTS OF AERODERIVATIVE COMBUSTOR TURBULENCE ON ENDWALL HEAT TRANSFER DISTRIBUTIONS ACQUIRED IN A LINEAR VANE CASCADEForrest E. Ames, Pierre A. Barbot, and Chao WangUniversity of North DakotaMechanical Engineering DepartmentGrand Forks, ND, USA
6  GT-2002-30094THE PREMIXED CONDITIONAL MOMENT CLOSURE METHOD APPLIED TO IDEALIZED LEAN PREMIXED GAS TURBINE COMBUSTORSScott M. MartinUniversity of WashingtonDepartment of Mechanical Engineering17136 Bak Rd.Belleville, MI 48111-3525734-699-6629 smmartin7@netscape.netJohn C. KramlichUniversity of WashingtonDepartment of Mechanical EngineeringBox 352600Seattle, WA 98195-2600206-543-5538 kramlich@me.washington.eduGeorge KosályUniversity of WashingtonDepartment of Mechanical Engineering206-543-6933 kosaly@me.washington.eduJames J. RileyUniversity of WashingtonDepartment of Mechanical Engineering206-543-5347 riley@me.washington.edu
7  GT-2002 -30597CFD ANALYSIS OF INDUSTRIAL GAS TURBINE EXHAUST DIFFUSERSV. Vassiliev S. Irmisch S. FlorjancicALSTOM (Switzerland) Ltd.Gas Turbines TurbomachineryBaden, Switzerland
8  GT-2002-30096VALIDATION OF A FLAMELET APPROACH TO MODELLING 3-DTURBULENT COMBUSTION WITHIN AN AIRSPRAY COMBUSTORA.G. KyneDepartment of Fuel and Energy, University ofLeeds, Leeds LS2 9JT, United Kingdom.C.W. WilsonCentre for Aerospace Technology, QinetiQ group plc,Cody Technology Park, Ively Road, Pyestock,Famborough, Hants, GU14 0LS, United KingdomM. PourkashanianDepartment of Fuel and Energy, University ofLeeds, Leeds LS2 9JT, United KingdomA. WilliamsDepartment of Fuel and Energy, University ofLeeds, Leeds LS2 9JT, United Kingdom
9  GT-2002-30218EFFECT OF ROTATION ON FLOW AND TEMPERATURE DISTRIBUTIONS IN A TWO-PASS CHANNEL CONNECTED BY TWO ROWS OF HOLESAchintya Pramanick and Srinath V. EkkadMechanical Engineering DepartmentLouisiana State UniversityBaton Rouge LA 70803
10  GT-2002-30069Experimental and Numerical Studies of the Velocity Field of a Triple Annular SwirlerGuoqiang Li and Ephraim J. GutmarkUniversity of CincinnatiDepartment of Aerospace Engineering and Engineering MechanicsCincinnati, Ohio 45221-0070, USATel: (513) 556-1227; Fax: (513) 556-5038; E-mail: Ephraim.Gutmark@uc.edu
11  GT-2002-30613FILM COOLING ON A MODERN HP TURBINE BLADEPART II: COMPOUND-ANGLE ROUND HOLESD. Keith Walters and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634Frederick A. BuckGE Aircraft EnginesCincinnati, OH 45215
12  GT-2002-30522FILM COOLING ON A MODERN HP TURBINE BLADEPART III: AXIAL SHAPED HOLESJeffrey D. Ferguson and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634Frederick A. BuckGE Aircraft EnginesCincinnati, OH 45215
13  GT-2002-30206PREDICTIONS OF EXTERNAL HEAT TRANSFER FOR TURBINE VANES AND BLADES WITH SECONDARY FLOWFIELDSK. Hermanson, S. Kern, G. Picker, S. ParneixAlstom Power (Schweiz)Im Segelhof 1CH-5405 Baden-D?ttwil, Switzerland
14  GT-2002-30396TOWARDS A REDUCTION OF COMPRESSOR BLADE DYNAMIC LOADING BY MEANS OF ROTOR-STATOR INTERACTION OPTIMIZATIONErnesto BeniniAndrea ToffoloDipartimento di Ingegneria MeccanicaUniversità di PadovaVia Venezia, 1 ? 35131 Padova (Italy)E-mail: {benini, toffolo}@dim.unipd.it
15  GT-2002-30616Two-Equation Versus Reynolds-Stress Modeling in Predicting Flow and Heat Transfer in a Smooth U-Duct with and without RotationX.Gu,H.-W.Wu,H.J.Schock,and T.I-P.ShihDepartment of Mechanical Engineering,Michigan State UniversityEast Lansing,Michigan,U.S.A.48824-1226
16  GT-2002-30480CFD Optimisation of Cooling Air Offtake Passages within Rotor CavitiesColin Young, Rolls-Royce plc, Derby, England. Guy D Snowsill, Rolls-Royce plc, Derby, England.
17  GT-2002-30049COMPUTATIONAL COMPARISON OF THE RB199 AND GE90 PYROMETER PURGING SYSTEMSClive Kerr Paul Ivey Neil OxleySchool Of EngineeringCranfield UniversityUnited KingdomSchool Of EngineeringCranfield UniversityUnited KingdomLand InfraredDronfieldUnited Kingdom
18  GT-2002-30188Effect of Non-Uniform Inlet Conditions on Endwall Secondary FlowsK. A. TholeMechanical Engineering DepartmentVirginia Polytechnic Institute and State UniversityBlacksburg, Virginia 24060USAK. S. HermansonAlstom PowerIm Segelhof 1CH - 5405 Baden-D?ttwilSwitzerland
19  GT-2002-30267HIGH CAPACITY AND HIGH EFFICIENCY MULTI-STAGE AIR INTAKE SYSTEMAlan Hashem, EITProduct ManagerMarine SystemsDani Fadda, Ph.D.CFD Engineering ScientistManager of Design AnalysisKenneth J. Fewel, P.E.Vice PresidentResearch and TechnologyPeerless Mfg. Co.Dallas, Texas
20  GT-2002-30479ICAS-GT: A EUROPEAN COLLABORATIVE RESEARCH PROGRAMME ON INTERNAL COOLING AIR SYSTEMS FOR GAS TURBINES.John W. ChewSchool of Mechanicaland Materials Engineering,University of Surrey,Guildford, Surrey, U.K.GU2 7XHPeter D. SmoutPerformance and Engine Systems,Rolls-Royce plc.,Derby, U.K.DE24 8BJPeter R. N. ChildsThermo-Fluid MechanicsResearch Centre,University of Sussex,Falmer, Sussex, U.K.BN1 9QT
21  GT-2002-30481MEASUREMENT AND ANALYSIS OF INGESTION THROUGH A TURBINE RIM SEALO. Gentilhomme, N. J. Hills, A. B. TurnerThermo-Fluid Mechanics Research CentreUniversity of SussexBrighton, East Sussex, BN1 9QT, UKJ. W. ChewFluids Research CentreSchool of EngineeringUniversity of SurreyGuildford, Surrey, GU2 7XH, UK
22  GT-2002-30524MEASUREMENT AND PREDICTION OF THE INFLUENCE OF CATALYTIC AND DRY LOW NOX  COMBUSTOR TURBULENCE ON VANE SURFACE HEAT TRANSFERForrest E. Ames, Chao Wang, and Pierre A. BarbotUniversity of North DakotaMechanical Engineering DepartmentGrand Forks, ND, USA
23  GT-2002-30470FILM COOLING ON A MODERN HP TURBINE BLADEPART I: EXPERIMENTAL & COMPUTATIONAL METHODOLOGY ANDVALIDATIONFrederick A. BuckGE Aircraft EnginesCincinnati, OH 45215D. Keith Walters, Jeffrey D. Ferguson, E. Lee McGrath, and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634
24  GT-2002-30166LEADING-EDGE FILM-COOLING PHYSICSART I - ADIABATIC EFFECTIVENESSWilliam D. York and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634
25  GT-2002-30520LEADING-EDGE FILM-COOLING PHYSICSART III - DIFFUSED HOLE EFFECTIVENESSWilliam D. York and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634
26  2002-GT-30674NUMERICAL INVESTIGATION OF VORTEX REDUCER FLOWS IN THEHIGH PRESSURE COMPRESSOR OF MODERN AEROENGINESDieter Peitsch, Manuela Stein, Stefan HeinRolls-Royce Deutschland Ltd. & Co. KGEschenweg 11D-15827 DahlewitzGermanyReinhard Niehuis, Ulf Reinm?llerInstitute of Jet Propulsion and TurbomachineryRheinisch-Westf?lische Technische HochschuleAachenTemplergraben 55D-52062 Aachen
27  GT-2002-30189PREDICTION AND MEASUREMENT OF THE FLOW AND HEAT TRANSFER ALONG THE ENDWALL AND WITHIN AN INLET VANE PASSAGEHugo D. PasinatoMechanical and Aerospace Engineering DepartmentArizona State UniversityTempe, Arizona 85287-6106Zan Liu and Ramendra P. RoyMechanical and Aerospace Engineering DepartmentArizona State UniversityTempe, Arizona 85287-6106W. Jeffrey HoweTurbines Advanced TechnologyHoneywell Engines and SystemsPhoenix, Arizona 85072-2181Kyle D. SquiresMechanical and Aerospace Engineering DepartmentArizona State UniversityTempe, Arizona 85287-6106Email: squires@asu.edu
28  GT-2002-30471PRESSURE-SIDE BLEED FILM COOLINGART I  STEADY FRAMEWORK FOR EXPERIMENTAL AND COMPUTATIONAL RESULTSD. Scott Holloway and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634Frederick A. BuckGE Aircraft EnginesCincinnati, OH 45215
29  GT-2002-30231A PREDICTION METHOD FOR THE LOCAL ENTROPY GENERATION RATE IN A TRANSITIONAL BOUNDARY LAYER WITH A FREE STREAM PRESSURE GRADIENTEd Walsh Roy MyoseStokes Research InstituteDepartment of Mechanical & Aeronautical EngineeringUniversity of LimerickPlassey Technological ParkLimerick, IrelandDepartment of Aerospace EngineeringWichita State UniversityWichita, KS 67260-0044, U.S.A.Mark DaviesStokes Research InstituteDepartment of Mechanical & Aeronautical EngineeringUniversity of LimerickPlassey Technological ParkLimerick, Ireland
30  GT-2002-30526COMBUSTOR TURBINE INTERFACE STUDIES - PART 1:ENDWALL EFFECTIVENESS MEASUREMENTSG. ZessPratt and Whitney400 Main Street M/S 163-01East Hartford, CT 06108W. F. Colban and K. A. TholeMechanical Engineering DepartmentVirginia Polytechnic Institute and State UniversityBlacksburg, Virginia 24061
31  GT-2002-30087DESIGN OF HIGH PERFORMING DUCT-BURNERS FOR COMBINED-CYCLE PLANTS USING PROGRESSIVE OPTIMIZATIONL. A. Catalano, A. Dadone, and D. ManodoroDipartimento di Ingegneria Meccanica e Gestionale & Centro di Eccellenza di Meccanica ComputazionalePolitecnico di Bari, via Re David 200, 70125, Bari, ItalyE-mails: catalano@poliba.it, dadone@imedado.poliba.it, manodoro@imedado.poliba.it
32  GT-2002-30182GAS TURBINE ENGINE DURABILITY IMPACTS OF HIGH FUEL-AIR RATIO COMBUSTORSPART 2: NEAR WALL REACTION EFFECTS ON FILM-COOLED HEAT TRANSFERDaniel R. Kirk1, Gerald R. Guenette2, Stephen P. Lukachko3, and Ian A. Waitz4Gas Turbine LaboratoryDepartment of Aeronautics and AstronauticsMassachusetts Institute of TechnologyCambridge, Massachusetts 02139
33  GT-2002-30167LEADING-EDGE FILM-COOLING PHYSICS:PART II - HEAT TRANSFER COEFFICIENTWilliam D. York and James H. LeylekDepartment of Mechanical EngineeringClemson UniversityClemson, SC 29634
34  GT-2002-30055TINTELL: AN INNOVATIVE METHOD FOR BLADE LIFE MANAGEMENTR. Hunik and R.A. RoothKEMA Nederland B.V.Arnhem, The Netherlands
35  GT-2002-30216NUMERICAL STUDY OF FLOW AND HEAT TRANSFER IN ROT TINGRECTANGULAR CHANNELS (AR =4)WITH 45 ??RIB TURBULATORS BYREYNOLDS STRESS TURBULENCE MODELMohammad Al-Qahtani Hamn-Ching Chen Je-Chin HanTurbine Heat Transfer LaboratoryDepartment of MechanicalEngineeringTexas A&M UniversityCollege Station,Texas 77843,USAOcean Engineering ProgramDepartment of CivilEngineeringTexas A&M UniversityCollege Station,Texas 77843,USATurbine Heat Transfer LaboratoryDepartment of MechanicalEngineeringTexas A&M UniversityCollege Station,Texas 77843,USA
36  GT-2002-30588AN UNDERGRADUATE GAS TURBINE ENGINE PROGRAM ENHANCED BY DESIGN AND RESEARCH THREADSLt Col Brenda A. HavenBrenda.Haven@usafa.af.milDr. Aaron R. ByerleyAaron.Byerley@usafa.af.milColonel D. Neal BarlowNeal.Barlow@usafa.af.milDepartment of AeronauticsUnited States Air Force Academy, CO 80840
37  GT-2002-30190FLOW AND HEAT TRANSFER PREDICTIONS FOR A FLAT-TIP TURBINE BLADEHuitao Yang Sumanta Acharya Srinath V. EkkadMechanical Engineering DepartmentLouisiana State University, Baton Rouge, LA, 70803Chander PrakashGE Aircraft Engines, Cincinnati, OH 45215Ron BunkerGE Corporate Research, Schenectady, NY 12309
38  GT-2002-30209HEAT TRANSFER ENHANCEMENT IN SQUARE DUCTS WITH V-SHAPED RIBS OF VARIOUS ANGLESRongguang Jia, Arash Saidi, and Bengt SundénDivision of Heat Transfer, P.O. Box 118Lund Institute of Technology221 00 Lund, Sweden
39  GT-2002-30082HIGH POWER DENSITY SILICON COMBUSTION SYSTEMS FOR MICRO GAS TURBINE ENGINESC.M.Spadaccini,J.Lee,S.Lukachko,I.A.WaitzGas Turbine LaboratoryDept.of Aeronautics and AstronauticsMassachusetts Institute of TechnologyCambridge,MA 02139A.MehraD-STAR Engineering Corp.Shelton,CT 06484X.ZhangDept.of Manufacturing Engineeringand Fraunhofer USA Center forManufacturing InnovationBoston UniversityBoston,MA 02115
40  GT-2002-30499IMPORTANCE OF INLET TOTAL PRESSURE CONDITIONS IN EVALUATINGPERFORMANCE OF NON-SYMMETRIC GAS TURBINE EXHAUST DUCTSM.H. CunninghamDepartment of MechanicalEngineeringQueen's UniversityKingston, ON, K7L 3N6A.M. BirkDepartment of MechanicalEngineeringQueen's UniversityKingston, ON, K7L 3N6W. Di BartolomeoPratt & Whitney CanadaLongueuil, Quebec, Canada.
41  GT-2002-30361MICRO AIR INJECTION AND ITS UNSTEADY RESPONSEIN A LOW-SPEED AXIAL COMPRESSORChaoqun Nie, Gang Xu, Xiaobin Cheng* and Jingyi ChenInstitute of Engineering Thermophysics, *Institute of AcousticsChinese Academy of SciencesBeijing, China
42  GT-2002-30600NUMERICAL INVESTIGATION OF THE EFFECT OF ASH PARTICLE DEPOSITION ON THE FLOW FIELD THROUGH TURBINE CASCADESHesham ElbatshInstitute of Thermal Turbomachines and PowerplantsVienna University of TechnologyHenmann HaselbacherInstitute of Thermal Turbomachines and powerplants
43  GT-2002-30553NUMERICAL SIMULATION OF FILM COOLING ON THE TIP OF A GAS TURBINE BLADESumanta Acharya Huitao Yang Srinath V. EkkadMechanical Engineering DepartmentLouisiana State University, Baton Rouge, LA, 70803Chander PrakashGE Aircraft Engines, Cincinnati, OH 45215Ron BunkerGE Corporate Research, Schenectady, NY 12309
44  GT-2002-30193NUMERICAL SIMULATION OF FLOW AND HEAT TRANSFER PAST A TURBINE BLADE WITH A SQUEALER-TIPHuitao Yang Sumanta Acharya Srinath V. EkkadMechanical Engineering DepartmentLouisiana State University, Baton Rouge, LA, 70803Chander PrakashGE Aircraft Engines, Cincinnati, OH 45215Ron BunkerGE Corporate Research, Schenectady, NY 12309


ASME2001年
1.John A. Verdicchio, John W. Chew, Nick J. Hills, Rolls-Royce plc., University of Surrey, University of Sussex. Coupled Fluid/Solid Heat Transfer Computation for Turbine Discs. ASME 2001-GT-0205
2.R. P. Roy, G.Xu, J. Feng, S. Kang, Arizona State University. Pressure Field and Main-Stream Gas Ingestion in a Rotor-Stator Disk Cavity. ASME 2001-GT-0564
3.Matthew J. Krerner, Savas Yavuzkurt, Pennsylvania State University. The Modeling and Analysis of a Package-Scale Circulation Fluidized Combustor. ASME 2001-GT-0002
4.X. Li, J. L. Gaddis, T. Wang, Clemson University, University of New Orleans. Mist/Stream Cooling by a Row of Impinging Jets. ASME 2001-GT-0151
5.Paulo C. Mancila, Pitschaiah Chakka, Sumanta Achar, Louisiana State University. Performance of a Trapped-Vortex Spray Combustor. ASME 2001-GT-0058
6.M. Bianco, B. Fortunato, S. M. Camporeale, Polytechnic University of Bari, University of Reggio Calabria. CFD Simulation of Humid Air Premixed Flame Combustion Chamber for Evaporative Gas Turbine Cycles. ASME 2001-GT-0061
7.F. A. Tap, J.P. Van Buijtenen, R. Modi, Delft University of Technology, Nuovo Pignone. Liquid Fuel Spray Characterization for the Design of the Dual-Fuel PGT10B Combustor. ASME 2001-GT-0044
8.K. K. Botros, G. R. Price, G. Kibrya, NOVA Research and Technology Corporation, Transcananda PipeLines Limited. Predictive Emission Monitoring Model for LM1600 Gas Turbines Based on Neural Network Architecture Trained on Field Measurements and CFD Data. ASME 2001-GT-0221
9.Nicholas J. Hills, Alan B. Turner, John W. Chew, University of Sussex, University of Surrey. Computational and Mathematical Modelling of Turbine Rim Seal Ingestion. ASME 2001-GT-0204
10.Ingo Forster, Eckhard Martens, Winfried-Hagen Friedl, Dieter Peitsch, University of Applied Science, Rolls-Royce Deutschland Ltd.. Numerical Study of Hot Gas Ingestion Into an Engine Type High-Pressure Turbine Rotor-Stator Cavity. ASME 2001-GT-0114
11.Dirnitrie Negulescu, Michael Pfitzner, Rolls-Royce Deutschland Ltd. And Company KG. Secondary Air Systems in Aeroengines Employing Vortex Reducers. ASME 2001-GT-0198
12.Toshihiko Takahashi, Kazunori Watanabe, Takeshi Takahashi, Central Research Institute of  Electric Power Industry. Transient Analyses of Conjugate Heat Transfer of a First Stage Rotor Blade in Start-Up and Shut-Down. ASME 2001-GT-0171
13.G. A. Zess, K. A. Thole, Virginia Polytechnic Institute and State University. Computational Design and Experimental Evaluation of Using a Leading Edge Fillet on a Gas Turbine Vane. ASME 2001-GT-0404
14.Soo-Yong Kim, A. Slitenko, Korea Institute of Machinery and Materials. Experimental Investigation of an Inert Gas Generator for Fire Suppressing. ASME 2001-GT-0412
15.Yumin Xiao, R. S. Amano, University of Wisconsin Milwaukee. Study of Losses in a Leakage Flow Through the Passage of Shrouded Turbine Blades With Swirl Velocity. ASME 2001-GT-0121
16.W. S. Cheung, J. R. Tilston, Defense Evaluation and Research Agency. Commissioning of a Test Rig for Auto-Ignition Delay Time Measurements on Kerosene Based Fuel Paper. ASME 2001-GT-0052
17.Mark K. Harrington, Marcus A. McWaters, David G. Bogard, Christopher A. Lemmon, Karen A. Thole, University of Texas Austin, University of Wisconsin-Madison, Virginia Polytechnic Inst. And State Univ. Full-Coverage Film Cooling With Short Normal Injection Holes. ASME 2001-GT-0130
18.Mohammad Al-Qahtani, Yong-Jun Jang, Hamn-Ching Chen, Je-Chin Han, Texas A&M University. Prediction of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels With 45 (degree) Rib Turbulators. ASME 2001-GT-0187

ASME2000年
1  2000-GT-350CFD PREDICTIONS AND FIELD MEASUREMENTS OF NOx EMISSIONSFROM LM1600 GAS TURBINE DURING PART LOAD OPERATIONG.R. Price, K.K. BotrosNOVA Research & Technology CentreCalgary, CanadaandG.M. GoldinFluent Inc.Lebanon, N.H., U.S.A.
2  2000-GT-0127DESIGN OF A JET-STIRRED GAS GENERATOR FOR STUDIES OFHIGH TEMPERATURE MIXING AND COMBUSTIONC. G. Fotache, D. J. Hautman, and T. J. RosfjordUnited Technologies Research CenterEast Hartford, CT 06108
3  2000-GT-0507RADIAL INFLOW INTO THE DOWNSTREAM CAVITY OF A COMPRESSOR STATOR WELLR.M. Scott, P.R.N. Childs, N.J. Hills, J.A. Millward*.Thermo-Fluid Mechanics Research Centre, School of EngineeringUniversity of Sussex, Brighton, United Kingdom*Rolls-Royce plc, Derby, United Kingdom
4  2000-GT-265Turbine Blade Entropy Generation RatePart I: The Boundary Layer DefinedM.R.D. Davies, F. K. O'Donnell & A.J. NivenPEI Technologies: Stokes Research InstituteDepartment Of Mechanical & Aeronautical EngineeringUniversity Of LimerickLimerick, Ireland
5  2000-GT-0519EFFECT OF TURBULENCE MODELING ON PARTICLE DISPERSIONAND DEPOSITION ON COMPRESSOR AND TURBINE BLADE SURFACESHesham El-BatshHermann HaselbacherInstitute of Thermal Turbomachines and PowerplantsVienna University ofTechnologyAustria
6  2000-GT-649EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION OF LOSSES IN ACIRCULAR TO OBLONG DIFFUSING GAS TURBINE TRANSITION DUCT WITHOFFSETA.J. Stronach A.M. BirkQueen's UniversityDepartment of Mechanical EngineeringMcLaughlin HallKingston, Ontario, CanadaPhone (613) 533-6843
7  2000-GT-198FLOW AND HEAT TRANSFER AT THE HUB ENDWALL OF INLETVANE PASSAGES -- EXPERIMENTS AND SIMULATIONSR.P. Roy, K.D. Squires, M. Gerendas, and S. SongMechanical and Aerospace EngineeringArizona State UniversityTempe, AZ 85287-6106(480) 965-1482roy@asu.eduW.J. Howe and A. AnsariAlliedSignal EnginesPhoenix, AZ 85072
8  2000-GT-0122INTEGRATED EXPERIMENTAL AND NUMERICAL APPROACH FOR FUEL-AIRMIXING PREDICTION IN A HEAVY-DUTY GAS TURBINE LP BURNERGiulio Mori, Sandro RazoreAnsaldo Ricerche s.r.l., Genova, ItalyMarina Ubaldi, Pietro ZuninoUniversità di Genova, DIMSET, Genova, Italy
9  2000-GT-242NOVEL BLADE COOLING ENGINEERING SOLUTIONSiegfried Moser, Mario Ivanisin, Jakob Woisetschl~ger, Herbert JerichaInstitute for Thermal Turbomachinery and Machine DynamicsTechnical University GrazInffeldgasse 25A-8010 Graz / Austria
10  2000-GT-0201HIGH FREESTREAM TURBULENCE EFFECTS ON ENDWALL HEAT TRANSFERFOR A GAS TURBINE STATOR VANER. W. Radomsky* and K. A. TholeMechanical Engineering DepartmentVirginia Polytechnic Institute and State UniversityBlacksburg, Virginia 24060
11  2000-GT-0135MODELING OF INHOMOGENEOUSLY PREMIXED COMBUSTIONWITH AN EXTENDED TFC MODELWolfgang PolifkeLehrstuhl A f ¨ ur ThermodynamikTechnical University of MunichD-85747 Garching, GermanyEmail: polifke@thermo-a.mw.tum.dePeter FlohrABB Alstom Power Technology Ltd.CH-5405 Baden, SwitzerlandEmail: peter.flohr@ch.abb.comMartin BrandtFachhochschule KarlsruheD-76133 Karlsruhe, Germany
12  2000-GT-0436Final PaperTRAILING EDGE 3D FREE SHEAR LAYERSN. Schrder, G. Hofmann, J. HourmouziadisJet Propulsion LaboratoryAerospace Institute F1Berlin University of TechnologyMarchstr. 12, D-10587 Berlin, Germanye-mail: Hourmouziadis@TU-Berlin.de
13  2000-GT-647EFFECT OF SWIRL ON THE PERFORMANCE OF A GAS TURBINEREVERSING EXHAUST DUCTM.H. Cunningham, A.M.BirkDepartment of Mechanical EngineeringQueen's UniversityKingston, Ontario, Canada.Phone (613) 533-2570J.E.D. GauthierDepartment of Mechanical EngineeringCarleton University,Ottawa, Ontario, Canada.W. Di BartolomeoPratt & Whitney CanadaLongueuil, Quebec, Canada.
14  2000-GT-633ON THE MODELING OF TIP LEAKAGE FLOWIN AXIAL TURBINE BLADE ROWSReinhard WillingerHermann HaselbacherInstitute of Thermal Turbomachines and PowerplantsVienna University of TechnologyAustria
15  2000-GT-251THERMAL CONJUGATE ANALYSIS OF A FIRST STAGE BLADE IN A GAS TURBINEToshihiko Takahashi Kazunori WatanabeTakeshi TakahashiCentral Research Institute of Electric Power IndustryYokosuka, Kanagawa, JAPAN
16  2000-GT-0147Computation of 3D Turbulent Not-premixed Reacting Flows Using an Implicit Unstructured SolverP. Adami and F. MartelliEnergetics Department S. Stecco- University of FlorenceVia S. Marta 3 ?50139 FlorenceTel.:+39 055 4796239 - Fax.:+39 055 4796342e-mail: adami@ing.unifi.it
17  2000-GT-0229Flow and Heat Transfer in a Rotating Square Channel with 45 o Angled Ribsby Reynolds Stress Turbulence ModelYong-Jun Jang Hamn -Ching Chen Je-Chin HanTurbine Heat Transfer Laboratory Ocean Engineering Program Turbine Heat Transfer LaboratoryDepartment of Mechanical Engineering Department of Civil Engineering Department of Mechanical EngineeringTexas A&M University Texas A&M University Texas A&M UniversityCollege Station, Texas 77843-3123 College Station, Texas 77843-3136 College Station, Texas 77843-3123
18  2000-GT-285FLOW AND HEAT TRANSFER IN AN INDUSTRIAL ROTOR-STATOR RIM SEALING CAVITYAlexander V. Mirzamoghadam and Zhenhua XiaoAdvanced Engine DevelopmentSiemens Westinghouse Power Corporation4400 Alafaya Trail, MC-205Orlando, FL. 32826
19  2000-GT-0117A NEW HYBRID AIR BLAST NOZZLE FOR ADVANCED GAS TURBINE COMBUSTORSAdel Mansour, Michael Benjamin, Erlendur SteinthorssonParker Hannifin Corporation, Gas Turbine Fuel Systems DivisonMentor, OH, 44060

redboy

很不错的,我们可以索要其中的论文么?

chen123yuhai

请问大X，你有2000届年会采用FLUENT软件发表的论文　　吗？或哪里可以下载啊
先谢过！

redboy

ASME2000~2002论文我这里有T类的
以前的谁有呀

haiyuanyuyy

redboy ，在哪里？

redboy

http://162.105.139.102/cgi-bin/LB5000/topic.cgi?forum=16&topic=208&show=0

布衣狂生

好

tintinxzl

请问斑竹，我怎样才能取得这些论文？

freedomlover

Verwendete Formeln:
(1) rho = D(j)
D = a(j) + D*T   {j von 4 bis 0}
a(0) = 999.84102229
a(1) = 0.067477741278
a(2) = -0.0089764830531
a(3) = 0.000088534831535
a(4) = -6.5515551052E-07
(2) rho = rho0 * (1 - p / K) ^ -1
rho0 = Dichte dest. Wasser in g/cm3 rho0 = 0.9998395 + 0.000067914 * T - 0.0000090894 * T * T + 0.00000010171 * T * T * T - 0.0000000012846 * T ^ 4 + 0.000000000011592 * T ^ 5 - 5.0125E-14 * T ^ 6 + (0.0008181-0.00000385 * T + 0.0000000496 * T * T) * S
K = 19652.17 + 148.113 * T * -2.293 * T * T + 0.01256 * T ^ 3 -0.0000418 * T ^ 4 + (3.2726 - 0.0002147 * T + 0.0001128 * T ^ 2) * p + (53.238 - 0.313 * T + 0.005728 * p) * S
(3) rho = 1 / ((1 - p/K) /R)
我只有密度函数

aguang

都可以下载吗