GT2010-22660 Study of Flow Control Using a Slotted Blade for a Compressor Airfoil at Low Reynolds Numbers (Englisch)
- Neue Suche nach: Zhou, M.
- Neue Suche nach: Zhu, J.
- Neue Suche nach: Lu, X.
- Neue Suche nach: Ge, Z.
- Neue Suche nach: Yan, K.
- Neue Suche nach: Huang, R.
- Neue Suche nach: Zhou, M.
- Neue Suche nach: Zhu, J.
- Neue Suche nach: Lu, X.
- Neue Suche nach: Ge, Z.
- Neue Suche nach: Yan, K.
- Neue Suche nach: Huang, R.
In:
ASME turbo expo
;
279-288
;
2010
-
ISBN:
- Aufsatz (Konferenz) / Print
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Titel:GT2010-22660 Study of Flow Control Using a Slotted Blade for a Compressor Airfoil at Low Reynolds Numbers
-
Beteiligte:
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Kongress:ASME turbo expo ; 2010 ; Glasgow
-
Erschienen in:ASME turbo expo ; 279-288PROCEEDINGS OF THE ASME TURBO EXPO ; 7a ; 279-288
-
Verlag:
- Neue Suche nach: ASME
-
Erscheinungsort:New York, N.Y.
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Erscheinungsdatum:01.01.2010
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Format / Umfang:10 pages
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Anmerkungen:Includes bibliographical references and author indexes
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ISBN:
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Medientyp:Aufsatz (Konferenz)
-
Format:Print
-
Sprache:Englisch
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Schlagwörter:
-
Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 1
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GT2010-22052 Comparative Studies of Alternative HPC Configurations for the NEWAC IRA EngineCalvert, W.J. / Swain, E. / Woods, I. / Dempsey, M. / Schmidt-Eisenlohr, U. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 11
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GT2010-22076 Assessment and Optimization of the Aerodynamic and Acoustic Characteristics of a Counter Rotating Open RotorSchnell, R. / Yin, J. / Voss, C. / Nicke, E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 27
-
GT2010-22079 Numerical Study of Wet Compression Using Methanol Injection in Axial CompressorEl-Said, A.F. / El-Salmawy, H.A. / Gobran, M.H. / Ragab, R.M.G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 39
-
GT2010-22082 The Influence of Tip Clearance on the Acoustic and Aerodynamic Characteristics of FansKarstadt, S. / Hess, M. / Matyschok, B. / Pelz, P.F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 49
-
GT2010-22092 Study of Tip Flows in High Hub-to-Tip Ratio Axial Compressors at Low Speed With Varying Tip Gaps, Inflow Conditions and Tip ShapesRoy, B. / Pradeep, A.M. / Suzith, A. / Bhatia, D. / Mulmule, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 63
-
GT2010-22101 Characteristics of Tip Clearance Flow Instability in a Transonic CompressorHah, C. / Voges, M. / Mueller, M. / Schiffer, H.-P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 75
-
GT2010-22106 An Experimental Investigation of Shrouded and Cantilevered Compressor Stators at Varying Clearance SizesLange, M. / Mailach, R. / Vogeler, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 87
-
GT2010-22142 Numerical Investigation Into the Unsteady Aerodynamics of a Ducted Helicopter Tail Rotor Under Side-Wind ConditionsKainz, M. / Danner, F. / Kau, H.-P. / Le Chuiton, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 99
-
GT2010-22153 Aerodynamic Research on the MCA-Type Compressor Blade CascadeSimurda, D. / Luxa, M. / Safarik, P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 109
-
GT2010-22187 Rotor Tip Flow-Fields Near Inception Point of Modal Disturbance in an Axial-Flow FanNishioka, T. / Kanno, T. / Hayami, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 121
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GT2010-22208 Effect of Surface Roughness Location and Reynolds Number on Compressor Cascade PerformanceBack, S.C. / Hobson, G.V. / Song, S.J. / Millsaps, K.T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 129
-
GT2010-22246 The Impact of Real Geometries on Three-Dimensional Separations in CompressorsGoodhand, M.N. / Miller, R.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 139
-
GT2010-22290 On Reliable Performance Prediction of Axial TurbomachinesHess, M. / Pelz, P.F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 151
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GT2010-22336 On the Efficiency of Secondary Flow Suction in a Compressor CascadeLiesner, K. / Lemke, M. / Meyer, R. / Gmelin, C. / Thiele, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 161
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GT2010-22345 Control of Tip-Clearance Flow in a Low Speed Axial Compressor Rotor With Plasma ActuationJothiprasad, G. / Murray, R.C. / Wadia, A. / Essenhigh, K. / Breeze-Stringfellow, A. / Bennett, G.A. / Saddoughi, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 173
-
GT2010-22365 CFD Analysis of Effects of Damage Due to Bird Strike on Fan PerformanceBohari, B. / Sayma, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 183
-
GT2010-22415 Study of Sand Particle Trajectories and Erosion Into the First Fan Stage of a TurbofanGhenaiet, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 203
-
GT2010-22439 Effect of a Gap Between Inner Casing and Stator Blade on Axial Compressor PerformanceLee, C. / Song, J. / Lee, S. / Hong, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 211
-
GT2010-22453 A Prediction Model for Corner Separation/Stall in Axial CompressorsYu, X. / Liu, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 223
-
GT2010-22464 Effects of Vortex Generator Application on the Performance of a Compressor CascadeHergt, A. / Meyer, R. / Engel, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 237
-
GT2010-22516 Unsteady RANS Simulations of a Highly Loaded Low Aspect Ratio Compressor Stator Cascade With Active Flow ControlGmelin, C. / Huppertz, A. / Steger, M. / Swoboda, M. / Thiele, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 247
-
GT2010-22569 Hot-Wire Measurements in a High Speed Counter Rotating Turbo Fan RigMeyer, R. / Knobloch, K. / Linden, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 255
-
GT2010-22578 Experimental Investigation of Endwall and Suction Side Blowing in a Highly Loaded Stator CascadeNerger, D. / Gummer, V. / Saathoff, H. / Clemen, C. / Radespiel, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 269
-
GT2010-22652 Investigation for the Effects of Circumferential Grooves on the Unsteadiness of Tip Clearance Flow to Enhance Compressor Flow InstabilityZhao, S. / Lu, X. / Zhu, J. / Zhang, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 279
-
GT2010-22660 Study of Flow Control Using a Slotted Blade for a Compressor Airfoil at Low Reynolds NumbersZhou, M. / Zhu, J. / Lu, X. / Ge, Z. / Yan, K. / Huang, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 289
-
GT2010-22704 Experimental and Numerical Analysis of Hub-Corner Stall in Compressor CascadesLewin, E. / Kozulovic, D. / Stark, U. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 301
-
GT2010-22721 Numerical Investigations of the Efficiency of Circulation Control in a Compressor StatorVorreiter, A. / Fischer, S. / Saathoff, H. / Radespiel, R. / Seume, J.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 317
-
GT2010-22792 Multidisciplinary 3D-Optimization of a Fan Stage Performance Map With Consideration of the Static and Dynamic Rotor MechanicsSiller, U. / Aulich, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 329
-
GT2010-22825 Results of an Advanced Fan Stage Operating Over a Wide Range of Speed and Bypass Ratio: Part I-Fan Stage Design and Experimental ResultsSuder, K.L. / Prahst, P.S. / Thorp, S.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 343
-
GT2010-22831 Experimental Investigation of the Aerodynamic Performance of a Linear Axial Compressor Cascade With Water Droplet LoadingEisfeld, T. / Joos, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 355
-
GT2010-22894 The Flow Field Within an Axial Flow Compressor at Extremely High Flow CoefficientsGill, A. / von Backstrom, T.W. / Harms, T.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 369
-
GT2010-22914 A Study of Fan-Distortion Interaction Within the NASA Rotor 67 Transonic StageFidalgo, V.J. / Hall, C.A. / Colin, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 381
-
GT2010-22923 Effect of Geometry Deviations on the Aerodynamic Performance of an Outlet Guide Vane CascadeChernoray, V. / Ore, S. / Larsson, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 391
-
GT2010-22952 Large Tip Clearance Flows in Two Compressor CascadesWilliams, R. / Ingram, G. / Gregory-Smith, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 403
-
GT2010-23056 The Internal Structure of the Tip Leakage Vortex Within the Rotor of an Axial Waterjet PumpMiorini, R.L. / Wu, H. / Katz, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 421
-
GT2010-23063 Experimental Study of Effects of Grooved Tip Clearances on the Flow Field in a Compressor Cascade PassageMa, H. / Zhang, J. / Zhou, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 431
-
GT2010-23116 The Highly Loaded Aerodynamic Design and Performance Enhancement of a Helium CompressorKe, T. / Zheng, Q. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 443
-
GT2010-23160 Numerical Study of the Stagger Angle Effects in Forward Swept Axial Compressor Rotor PassagesRamakrishna, P.V. / Govardhan, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 455
-
GT2010-23244 Investigation of Compressor Tip Clearance Flow StructureMatzgeller, R. / Burgold, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 465
-
GT2010-23386 Results of an Advanced Fan Stage Over a Wide Operating Range of Speed and Bypass Ratio: Part II - Comparison of CFD and Experimental ResultsCelestina, M.L. / Suder, K.L. / Kulkarni, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 477
-
GT2010-23404 The Effect of an Upstream Compressor on a Non-Axisymmetric S-DuctKarakasis, M.K. / Naylor, E.M.J. / Miller, R.J. / Hodson, H.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 487
-
GT2010-23474 Experimental Investigation of the Steady and Unsteady Flow Field in a Single Stage Low Pressure Axial Compressor With a Circumferential Groove Casing TreatmentVan de Wyer, N. / Farkas, B. / Desset, J. / Brouckaert, J.F. / Thomas, J.-F. / Hiernaux, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 501
-
GT2010-23516 An Experimental and Computational Investigation of Tip Clearance Flow and Its Impact on Stall InceptionBennington, M.A. / Ross, M.H. / Cameron, J.D. / Morris, S.C. / Du, J. / Lin, F. / Chen, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 513
-
GT2010-23606 A CFD Study of Circumferential Groove Casing Treatments in a Transonic Axial CompressorChen, H. / Huang, X. / Shi, K. / Fu, S. / Bennington, M.A. / Morris, S.C. / Ross, M. / McNulty, S. / Wadia, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 525
-
GT2010-23608 Numerical Study of Discrete Tip Injection in a Transonic Axial CompressorKhaleghi, H. / Teixeira, J.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 537
-
GT2010-22049 3D Direct and Inverse Design Using NS Equations and the Adjoint Method for Turbine BladesWang, D.X. / Li, Y.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 547
-
GT2010-22061 Secondary Flow Reduction by Blade Redesign and Endwall Contouring Using an Adjoint Optimization MethodLuo, J. / Xiong, J. / Liu, F. / McBean, I. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 563
-
GT2010-22107 An Analysis of the Merits of CFD for the Performance Prediction of a Low Pressure Steam Turbine Radial DiffuserBeevers, A. / Congiu, F. / Pengue, F. / Mokulys, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 575
-
GT2010-22141 Two Dimensional Optimization of Centrifugal Compressor Impellers Using Online Quasi-3D Flow Solver and Genetic AlgorithmMa, Y. / Engeda, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 587
-
GT2010-22176 Ad-Hoc Boundary Conditions for CFD Analyses of Turbomachinery Problems With Strong Radial Flow Gradients at Farfield BoundariesCampobasso, M.S. / Baba-Ahmadi, M.H. / McLelland, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 601
-
GT2010-22194 Demonstration of an Aerodynamic Design Process for Turbomachines Using Open Source Software ToolsBorm, O. / Balassa, B. / Barthmes, S. / Fellerhoff, J. / Kuhrmann, A. / Kau, H.-P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 613
-
GT2010-22207 Computation of Laminar-Turbulent Transition in Turbumachinery Using the Correlation Based gamma -Re~ ~t~h~e~t~a~ Transition ModelKelterer, M.E. / Pecnik, R. / Sanz, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 623
-
GT2010-22228 Framework for Multidisciplinary Optimization of TurbomachineryTurner, M.G. / Park, K. / Siddappaji, K. / Dey, S. / Gutzwiller, D.P. / Merchant, A. / Bruna, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 633
-
GT2010-22229 Blade Geometry Optimization for Axial Flow CompressorZheng, R. / Xiang, J. / Sun, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 645
-
GT2010-22239 Development in Gas Turbine RepairsThomson, A. / Anderton, D.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 653
-
GT2010-22370 Attenuation of Vane Distortion in a Transonic Turbine Using Optimization Strategies: Part 1 - MethodologyJoly, M. / Verstraete, T. / Paniagua, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 663
-
GT2010-22371 Attenuation of Vane Distortion in a Transonic Turbine Using Optimization Strategies: Part II - OptimizationJoly, M. / Paniagua, G. / Verstraete, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 673
-
GT2010-22378 Minimizing Inlet Distortion for Hybrid Wing Body AircraftLiou, M.-S. / Lee, B.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 687
-
GT2010-22396 Design Optimization of Circumferential Casing Grooves for a Transonic Axial Compressor to Enhance Stall MarginChoi, K.-J. / Kim, J.-H. / Kim, K.-Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 697
-
GT2010-22469 Steady/Unsteady Reynolds Averaged Navier-Stokes and Large Eddy Simulations of a Turbine Blade at High Subsonic Outlet Mach NumberLeonard, T. / Duchaine, F. / Gourdain, N. / Gicquel, L.Y.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 711
-
GT2010-22482 Towards Cooled Turbine Life Prediction via Concurrent Aerodynamic, Thermal and Material Stress Simulations on Conjugate MeshesDawes, W.N. / Kellar, W.P. / Harvey, S.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 723
-
GT2010-22513 3D Simulation of Coupled Fluid Flow and Solid Heat Conduction for the Calculation of Blade Wall Temperature in a Turbine StageWlassow, F. / Duchaine, F. / Leroy, G. / Gourdain, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 735
-
GT2010-22540 Some Limitations of Turbomachinery CFDDenton, J.D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 747
-
GT2010-22543 Aeroacoustics and Performance Modeling of a Counter-Rotating PropfanOlausson, M. / Avellan, R. / Sorman, N. / Rudebeck, F. / Eriksson, L.-E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 757
-
GT2010-22588 Multi-Objective Design Optimisation of a Diffuser-Ejector Exhaust Duct for Helicopter EnginesGrasel, J. / Demolis, J. / Mohr, H. / Schiffer, H.-P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 771
-
GT2010-22627 Numerical Benchmark of Turbulence Modelling in Gas Turbine Rotor-Stator SystemDa Soghe, R. / Innocenti, L. / Andreini, A. / Poncet, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 785
-
GT2010-22655 Multi-Objective Optimization Design Method for Tandem Compressor Cascade at Design and Off Design ConditionsJu, Y. / Zhang, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 797
-
GT2010-22730 An Assessment of Non-Intrusive Probabilistic Methods for Turbomachinery ProblemsShankaran, S. / Barr, B. / Mallina, R. / Avancha, R. / Stein, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 807
-
GT2010-22793 Advanced Numerical Simulation Dedicated to the Prediction of Heat Transfer in a Highly Loaded Turbine Guide VaneGourdain, N. / Duchaine, F. / Collado, E. / Gicquel, L.Y.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 821
-
GT2010-22795 Euler Inverse Axisymmetric Solution for Design of Axial Flow Multistage TurbomachineryTaddei, S.R. / Bertini, F. / Larocca, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 831
-
GT2010-22841 Towards a High Order Throughflow: Part I - Investigating the Effectiveness of a Harmonic Reconstruction for 3D FlowsThomas, J.P. / Leonard, O. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 843
-
GT2010-22842 Towards a High Order Throughflow: Part II - Investigation of the Nonlinear Harmonic Method Coupled With an Immersed Boundary Method for the Modeling of the Circumferential StressesThomas, J.P. / Leonard, O. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 855
-
GT2010-22918 Uncertainty Analysis for Large-Scale Industrial Radial CompressorsBuche, D. / Beetz, M. / Ribi, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 865
-
GT2010-22940 Time-Linearized and Time-Accurate 3D RANS Methods for Aeroelastic Analysis in TurbomachineryKersken, H.-P. / Frey, C. / Voigt, C. / Ashcroft, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 875
-
GT2010-23011 Optimization of a Gas Turbine Engine Rotor Disc Using Case-Based Reasoning and the GATE Genetic AlgorithmDominique, S. / Trepanier, J.-Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 889
-
GT2010-23133 Discontinuous Galerkin Solution of Three-Dimensional Reynolds-Averaged Navier-Stokes Equations With S-A Turbulence ModelFeng, F. / Gu, C. / Li, X. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 897
-
GT2010-23239 Prediction of Separation-Induced Transition Using a Correlation-Based Transition ModelCorral, R. / Gisbert, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 909
-
GT2010-23284 Redesign of High-Lift LP-Turbine Airfoils for Low Speed TestingMarconcini, M. / Rubechini, F. / Pacciani, R. / Arnone, A. / Bertini, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 919
-
GT2010-23341 A Novel Quasi 3-D Design Method for Centrifugal Compressor Meridional PlaneNili-Ahmadabadi, M. / Durali, M. / Hajilouy-Benisi, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 933
-
GT2010-23390 A Dual-Mesh Approach to Enhance Accuracy of the Boundary Conditions for Unstructured Grid Modeling of Turbomachinery FlowsYang, H. / Jiang, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 943
-
GT2010-23399 On the Use of Blades Stagger and Stacking in Turbine Stage OptimizationArabnia, M. / Ghaly, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 957
-
GT2010-23400 Dual Point Redesign of an Axial Compressor Airfoil Using a Viscous Inverse Design MethodRamamurthy, R. / Ghaly, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 967
-
GT2010-23406 Aero-Structural Optimization of an Axial Turbine Stage in Three-Dimensional FlowSivashanmugam, V.K. / Arabnia, M. / Ghaly, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 981
-
GT2010-23414 A Generalized Axisymmetric Boundary Condition Method for Parallel Unstructured Field SolversHyams, D.G. / Webster, R. / Sreenivas, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 997
-
GT2010-23431 Hybrid Les Approach for Practical Turbomachinery Flows: Part 1 - Hierarchy and Example SimulationsTucker, P. / Eastwood, S. / Klostermeier, C. / Jefferson-Loveday, R. / Tyacke, J. / Liu, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1011
-
GT2010-23593 Numerical Simulation of Sand Erosion in a Transonic Compressor RotorSuzuki, M. / Yamamoto, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1019
-
GT2010-23627 Benchmarking CD-ADAPCO's Star-CCM+ in a Production Design EnvironmentGrigoriev, M.M. / Swiatek, C.V. / Hitt, J.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1027
-
GT2010-23714 Study on Aerodynamic Redesign of a High Pressure Ratio Centrifugal CompressorZhang, C. / Deng, Q. / Feng, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1041
-
GT2010-23775 Two Schemes of Multi-Objective Aerodynamic Optimization for Centrifugal Impeller Using Response Surface Model and Genetic AlgorithmLiu, X. / Zhang, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1055
-
GT2010-23807 Hybrid Les Approach for Practical Turbomachinery Flows: Part 2 - Further ApplicationsTucker, P.G. / Eastwood, S. / Klostermeier, C. / Xia, H. / Tyacke, J. / Ray, P. / Dawes, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1069
-
GT2010-22006 The Performance of a Generic Non-Axisymmetric Endwall in a Single Stage, Rotating Turbine at On and Off-Design ConditionsSnedden, G. / Dunn, D. / Ingram, G. / Gregory-Smith, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1081
-
GT2010-22056 Improvement of Cooled Turbine Airfoils by Special CutbackMamaev, B.I. / Petukhovskiy, M.M. / Pozdnyakov, A.V. / Valeev, M.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1089
-
GT2010-22065 Influence of Chord Length and Inlet Boundary Layer on the Secondary Losses of Turbine BladesSauer, H. / Schmidt, R. / Vogeler, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1101
-
GT2010-22088 Study of Gas Turbine Exhaust Diffuser Performance and its Enhancement by Shape ModificationsPradeep, A.M. / Roy, B. / Vaibhav, V. / Srinuvasu, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1111
-
GT2010-22134 Effects of Blade Loading Distribution on Aerodynamic Performance of Ultra-High Lift LP Turbine Airfoils Under the Influences of Wake Passing and Freestream TurbulenceFunazaki, K.-i. / Shiba, T. / Tanimitsu, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1123
-
GT2010-22205 The Influence of Different Rim Seal Geometries on Hot-Gas Ingestion and Total Pressure Loss in a Low-Pressure TurbineSchuler, P. / Kurz, W. / Dullenkopf, K. / Bauer, H.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1135
-
GT2010-22240 ``Online Throughflow'': Automatic Simultaneous Simulation of an Axial Flow TurbineSchinko, N. / Marx, M. / Rose, M.G. / Staudacher, S. / Gier, J. / Hubner, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1145
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GT2010-22328 Investigation of Low Solidity LP Turbine Cascade With Flow Control: Part 1 - Active Flow Control Using Jet-FlapChen, P.-P. / Qiao, W.-Y. / Luo, H.-L. / Hashmi, F.A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1155
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GT2010-22330 Investigation of Low Solidity LP Turbine Cascade With Flow Control: Part 2 - Passive Flow Control Using Gurney-FlapChen, P.-P. / Qiao, W.-Y. / Luo, H.-L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1163
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GT2010-22363 Numerical Simulation of a Highly Loaded LPT Cascade With Strong Suction Side Separation Under Periodically Unsteady Inflow ConditionsSchwarze, M. / Niehuis, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1177
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GT2010-22448 Improving the Interaction Between Leakage Flows and Main Flow in a Low Pressure TurbineMahle, I. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1187
-
GT2010-22449 Design and Analysis of HP-Turbine for Variable Cycle EngineLiu, Z.-g. / Fang, X.-j. / Liu, S.-y. / Wang, P. / Zhao, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1197
-
GT2010-22481 The Influence of the Total Pressure Profile on the Performance of Axial Gas Turbine DiffusersHirschmann, A. / Volkmer, S. / Schatz, M. / Finzel, C. / Casey, M. / Montgomery, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1209
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GT2010-22487 Quantitative Risk Assessment for the Performance Estimation of a Gas Turbine UpgradeHeinze, S. / Tageman, K. / Klang, A. / Molker, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1221
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GT2010-22490 On the Development of Short Axial Length Turbine Stator With Outlet Mach Number 2Nemec, M. / Straka, P. / Jelinek, T. / Babak, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1231
-
GT2010-22541 The Effect of Clearance on Shrouded and Unshrouded Turbines at Two Levels of ReactionYoon, S. / Curtis, E. / Denton, J. / Longley, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1243
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GT2010-22566 Characteristics of Tip Leakage Flow of the Turbine Blades With Cutback Squealer and Coolant InjectionWang, J. / Liu, Y. / Wang, X. / Du, Z. / Yang, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1253
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GT2010-22587 Numerical Investigations of Flow Separation Control for a Low Pressure Turbine Blade Using Steady and Pulsed Vortex Generator JetsXiaomin, L. / Zhou, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1263
-
GT2010-22594 Complex Secondary Flow and Associated Loss Generation in Ultra-Highly Loaded Turbine CascadeTsujita, H. / Yamamoto, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1275
-
GT2010-22674 Aerodynamic Analysis and Redesign of an Inlet Segment for a Heavy-Duty Gas Turbine EngineAbdel-Wahab, S. / Vogel, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1283
-
GT2010-22675 Predicting the Profile Loss of High-Lift Low Pressure TurbinesCoull, J.D. / Hodson, H.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1299
-
GT2010-22727 Measurements of Losses and Reynolds Stresses in the Secondary Flow Downstream of a Low-Speed Linear Turbine CascadeMaclsaac, G.D. / Sjolander, S.A. / Praisner, T.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1315
-
GT2010-22739 Passive Boundary Layer Control on a Highly Loaded Low Pressure Turbine CascadeMartinstetter, M. / Niehuis, R. / Franke, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1327
-
GT2010-22759 Measurements of Endwall Flows in Transonic Linear Turbine Cascades: Part I - Low Flow TurningTaremi, F. / Sjolander, S.A. / Praisner, T.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1343
-
GT2010-22760 Measurements of Endwall Flows in Transonic Linear Turbine Cascades: Part II - High Flow TurningTaremi, F. / Sjolander, S.A. / Praisner, T.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1357
-
GT2010-22765 The Effect of Reynolds and Mach Number on End-Wall Profiling PerformanceVazquez, R. / Fidalgo, V.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1369
-
GT2010-22773 Impact of Flowfield Unsteadiness on Film Cooling of a High Pressure Turbine BladeVitt, P. / Iverson, C. / Malak, M.F. / Liu, J.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1381
-
GT2010-22783 Numerical Simulation of Clocking Effect on Wake Transportation and Interaction in a 1.5-Stage Axial TurbineWei, L. / Hua, O. / Du, Z.-h. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1391
-
GT2010-22810 Investigation of Aerodynamic Losses and Film Cooling Effectiveness for a NGV ProfileStephan, B. / Kruckels, J. / Gritsch, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1401
-
GT2010-22840 Impact of the Inflow Conditions on the Heavy-Duty Gas Turbine Exhaust Diffusers PerformanceVassiliev, V. / Irmisch, S. / Abdel-Wahab, S. / Granovskiy, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1413
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GT2010-22843 Effects of an Upstream Cavity on the Secondary Flow in a Transonic Turbine CascadeEl Ella, H.M.A. / Sjolander, S.A. / Praisner, T.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1425
-
GT2010-22876 Parametrical Investigation of Turbine Stages With Open Tip Clearance for the Purpose of Stage Efficiency IncreaseGranovskiy, A. / Kostege, M. / Lomakin, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1433
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GT2010-22884 Aerodynamic Performance of a Very High Lift Low Pressure Turbine Airfoil (T106C) at Low Reynolds and High Mach Number With Effect of Free Stream Turbulence IntensityMichalek, J. / Monaldi, M. / Arts, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1445
-
GT2010-22892 The Application of Low-Profile Vortex Generators in an Intermediate Turbine DiffuserSantner, C. / Gottlich, E. / Marn, A. / Hubinka, J. / Paradiso, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1457
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GT2010-22901 Performance of a Nozzle Guide Vane in Subsonic and Transonic Regimes Tested in an Annular SectorYasa, T. / Paniagua, G. / Fridh, J. / Vogt, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1469
-
GT2010-22971 Part-Span Application of Sweep and Lean at Turbine Blade Tips: A Low Speed Experimental Cascade StudyRoy, B. / Prajapati, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1479
-
GT2010-23114 LP Turbine Reynolds Lapse Phenomena: Time Averaged Area Traverse and Multistage CFDKurner, M. / Schneider, C. / Rose, M.G. / Staudacher, S. / Gier, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1489
-
GT2010-23123 Study of Viscous Controlled Vortex Design of a LP Turbine StageZheng, Q. / Gao, J. / Li, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1503
-
GT2010-23166 Optical Investigation of Profile Losses Coefficient in a Linear Turbine CascadeAlhaj, O. / Seume, J.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1515
-
GT2010-23222 The Interaction Between Horseshoe Vortex and Longitudinal Vortices From the Vortex GeneratorsAndoh, M. / Motosuke, M. / Honami, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1525
-
GT2010-23300 A CFD Study of Low Reynolds Number Flow in High Lift CascadesPacciani, R. / Marconcini, M. / Arnone, A. / Bertini, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1535
-
GT2010-23317 Effect of Surface Roughness on Loss Behaviour: Aerodynamic Loading and Boundary Layer Development of a Low-Pressure Gas Turbine AirfoilMontis, M. / Niehuis, R. / Fiala, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1549
-
GT2010-23350 Numerical and Experimental Analysis of the Effects of Non-Axisymmetric Contoured Stator Endwalls in an Axial TurbinePoehler, T. / Gier, J. / Jeschke, P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1561
-
GT2010-23461 Numerical Investigation of the Influence of Real World Blade Profile Variations on the Aerodynamic Performance of Transonic Nozzle Guide VanesEdwards, R. / Asghar, A. / Woodason, R. / LaViolette, M. / Boulama, K.G. / Allan, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1571
-
GT2010-23475 Wake Control by Boundary Layer Suction Applied to a High-Lift Low-Pressure Turbine BladeSatta, F. / Ubaldi, M. / Zunino, P. / Schipani, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1583
-
GT2010-23491 A Simplified Method With Local Correlations for the Analysis of Multistage Axial TurbinesRatto, L. / Satta, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1593
-
GT2010-23542 Aeromechanical Optimisation of a Winglet-Squealer Tip for an Axial TurbineSchabowski, Z. / Hodson, H. / Giacche, D. / Power, B. / Stokes, M.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1609
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GT2010-23552 Combined Blowing and Suction to Control Both Midspan and Endwall Losses in a Turbomachinery PassageBloxham, M.J. / Bons, J.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1619
-
GT2010-23564 Experimental and Numerical Investigations of Aerodyanmic Behavior of a Three-Stage HP-Turbine at Different Operating ConditionsAbdelfattah, S.A. / Schobeiri, M.T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1633
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GT2010-23591 Highly Loaded Low-Pressure Turbine: Design, Numerical, and Experimental AnalysisSchmitz, J.T. / Morris, S.C. / Ma, R. / Corke, T.C. / Clark, J.P. / Koch, P.J. / Puterbaugh, S.L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1647
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GT2010-23604 Computational Study of Geometric Parameter Influence on Aggressive Inter-Turbine Duct PerformanceCouey, P.T. / McKeever, C.W. / Malak, M.F. / Srinivasan, B. / Ramachandran, D. / Hasti, R.V. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1657
-
GT2010-23721 Influence of Rotor Blade Fillets on Aerodynamic Performance of Turbine StageShi, Y. / Li, J. / Feng, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1669
-
GT2010-23808 Experimental and Numerical Studies on Highly Loaded Supersonic Axial Turbine CascadesWolf, T. / Kost, F. / Janke, E. / Haselbach, F. / Willer, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1677
-
GT2010-22038 Performance Test Diagnosis of a Compact Two Stage High Pressure Ratio CompressorRodgers, C. / Brown, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1687
-
GT2010-22138 Parker-Type Acoustic Resonances in the Return Guide Vane Cascade of a Centrifugal Compressor: Theoretical Modelling and Experimental VerificationKonig, S. / Petry, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1701
-
GT2010-22154 An Investigation of Compressor Map Width Enhancement and the Inducer Flow Field Using Various Configurations of Shroud Bleed SlotSivagnanasundaram, S. / Spence, S. / Early, J. / Nikpour, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1711
-
GT2010-22164 Analysis and Validation of a Unified Slip Factor Model for Impellers at Design and Off-Design ConditionsQiu, X. / Japikse, D. / Zhao, J. / Anderson, M.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1723
-
GT2010-22177 The Effects of Radial Inlet on the Performance of Variable Inlet Guide Vanes in a Centrifugal Compressor StageTan, J. / Qi, D. / Wang, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1733
-
GT2010-22212 The Effect of Unequal Admission on the Performance and Loss Generation in a Double-Entry Turbocharger TurbineCopeland, C.D. / Newton, P. / Seiler, M. / Martinez-Botas, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1747
-
GT2010-22222 Development of a Rotating Centrifugal Separator Technology for Centrifugal CompressorsMaier, W. / Chochua, G. / Biba, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1757
-
GT2010-22281 Effect of Impeller Blade Loading on Compressor Stage Performance in a High Specific Speed RangeShibata, T. / Yagi, M. / Nishida, H. / Kobayashi, H. / Tanaka, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1769
-
GT2010-22283 Compressor Design for Multi-Point Operating Conditions of Turbocharged Gasoline EnginesChen, T. / Zhang, Y. / Zheng, X. / Zhuge, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1779
-
GT2010-22366 Numerical Characterization of the Inlet Flow for Eleven Radial TurbomachinesPackard, N.O. / Japikse, D. / Maynes, R.D. / Gorrell, S.E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1793
-
GT2010-22381 Impact of Fan Gap Flow to the Centrifugal Impeller AerodynamicsLee, Y.-T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1805
-
GT2010-22394 Unsteady Behavior and Control of Diffuser Leading-Edge Vortex in a Centrifugal CompressorOhta, Y. / Goto, T. / Outa, E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1815
-
GT2010-22417 Simulation of Particle Trajectories and Erosion Through a Centrifugal CompressorGhenaiet, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1831
-
GT2010-22419 Prediction of Erosion in Radial Turbine ComponentsGhenaiet, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1847
-
GT2010-22506 Extracting Two-Zone Model Parameters for Centrifugal Compressor DesignGu, F. / Thilges, C. / Cambio, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1859
-
GT2010-22549 The Cordier Line for Mixed Flow CompressorsCasey, M. / Zwyssig, C. / Robinson, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1871
-
GT2010-22557 Blade Thickness Effect on Impeller Slip FactorZhang, D. / Di Liberti, J.-L. / Cave, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1879
-
GT2010-22570 Effect of Recirculation Device on Performance of High Pressure Ratio Centrifugal CompressorTamaki, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1891
-
GT2010-22581 Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control: Part I - Non-Axisymmetric Flow in Centrifugal CompressorYang, M. / Zheng, X. / Zhang, Y. / Bamba, T. / Tamaki, H. / Huenteler, J. / Li, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1903
-
GT2010-22582 Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control: Part II - Non-Axisymmetric Self Recirculation Casing TreatmentZheng, X. / Zhang, Y. / Yang, M. / Bamba, T. / Tamaki, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1913
-
GT2010-22605 Study of the Flow in a Vaneless Diffuser at Part Speed Operating ConditionsHazby, H.R. / Xu, L. / Schleer, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1925
-
GT2010-22622 A 3-D Compressible Flow Model for Weak Rotating Waves in Vaneless Diffusers: Part I - The ModelChen, H. / Shen, F. / Zhu, X.-c. / Du, Z.-h. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1937
-
GT2010-22666 Validation and Development of Loss Models for Small Size Radial TurbinesSuhrmann, J.F. / Peitsch, D. / Gugau, M. / Heuer, T. / Tomm, U. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1951
-
GT2010-22669 A Numerical Study of the Flow Fields in a Highly Off-Design Variable Geometry TurbineWalkingshaw, J. / Spence, S. / Ehrhard, J. / Thornhill, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1961
-
GT2010-22737 Investigation of Unsteady Impeller-Diffuser Interaction in a Transonic Centrifugal Compressor StageLiu, Y. / Liu, B. / Lu, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1973
-
GT2010-22861 Analysis of Secondary Flow Behavior in Low Solidity Cascade Diffuser of a Centrifugal BlowerIshida, M. / Murakami, T. / Sakaguchi, D. / Ueki, H. / Hayami, H. / Senoo, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1983
-
GT2010-22883 Experimental Study of Vaned Diffusers in Centrifugal CompressorJaatinen, A. / Gronman, A.-P. / Turunen-Saaresti, T. / Backman, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 1997
-
GT2010-22913 Steady and Transient Computations of Interaction Effects in a Centrifugal Compressor With Different Types of DiffusersAnish, S. / Sitaram, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2007
-
GT2010-23019 Optimizing a Suction Channel to Improve Performance of a Centrifugal Compressor StageYagi, M. / Shibata, T. / Nishida, H. / Kobayashi, H. / Tanaka, M. / Sugimura, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2019
-
GT2010-23048 Novel IGV Designs for Centrifugal Compressors and Their Interaction With the ImpellerMohseni, A. / Goldhahn, E. / Van den Braembussche, R.A. / Seume, J.R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2031
-
GT2010-23096 Numerical Investigation on the Labyrinth Seal Design for a Low Flow Coefficient Centrifugal CompressorWang, Z. / Xu, L. / Xi, G. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2043
-
GT2010-23112 Aerodynamic Analysis of a Micro Turbine Centrifugal CompressorOlivero, M. / Javed, A. / van Buijtenen, J.P. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2053
-
GT2010-23345 Comparative Study on Tip Clearance Flow Fields in Two Types of Transonic Centrifugal Compressor Impeller With Splitter BladesYamada, K. / Tamagawa, Y. / Fukushima, H. / Furukawa, M. / Ibaraki, S. / Iwakiri, K.-i. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2065
-
GT2010-23457 A New Type of Self-Adaptive Casing Treatment for a Centrifugal CompressorWang, T. / Xu, W. / Gu, C. / Xiao, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2075
-
GT2010-23677 Unsteady Rotor-Stator Interaction of a Radial-Inflow Turbine With Variable Nozzle VanesKawakubo, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2085
-
GT2010-22003 Unsteady Forces of Rotor Blades in Full and Partial Admission TurbinesHushmandi, N.B. / Fridh, J.E. / Fransson, T.H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2099
-
GT2010-22026 Aerodynamic Optimization of an Impulse Turbine Cascade Including Laminar/Turbulent Transition PredictionBenini, E. / da Ronco, C.C. / Ponza, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2109
-
GT2010-22165 Aerodynamic Design of Transonic Tip SectionsStein, A. / Hofer, D.C. / Filippenko, V. / Slepski, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2119
-
GT2010-22183 Semi-Analytical Procedure for Prediction of Radial Clearances in Industrial Steam TurbinesHesse, C. / Schoene, S. / Gampe, U. / Kober, J. / Fogt, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2127
-
GT2010-22279 Effects of Design Variations of Rotor Entry Cavity Geometry on Shrouded Steam Turbine PerformanceBarmpalias, K.G. / Kalfas, A.I. / Abhari, R.S. / Hirano, T. / Shibukawa, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2139
-
GT2010-22280 Aerodynamic Optimization System Development for Low Pressure Exhaust Hood of Steam TurbineWang, H. / Zhu, X. / Du, Z. / Hong, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2149
-
GT2010-22312 Three-Dimensional Design Method for Long Blades of Steam Turbines Using Fourth-Degree NURBS SurfaceSenoo, S. / Ogata, K. / Nakamura, T. / Shibashita, N. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2159
-
GT2010-22316 Investigations of Influential Factors on the Aerodynamic Performance of a Steam Turbine Exhaust SystemFu, J.-L. / Liu, J.-J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2171
-
GT2010-22317 Steam Turbine Design Considerations for Ultrasupercritical CyclesZachary, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2181
-
GT2010-22391 Reduction of Pressure Forces in Turbine Labyrinth SealsKosowski, K. / Stepien, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2199
-
GT2010-22467 Non-Equilibrium Condensation Effects on the Flow Field and the Performance of a Low Pressure Steam TurbineStarzmann, J. / Casey, M. / Sieverding, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2209
-
GT2010-22477 A CFD Approach to Fluid Dynamic Optimum Design of Steam Turbine Stages With Stator and Rotor BladesYuan, X. / Tanuma, T. / Zhu, X. / Lin, Z. / Nomura, D. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2219
-
GT2010-22608 Rotor Dynamic Analysis on Partial Admission Control Stage in a Large Power Steam TurbineGao, L. / Dai, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2227
-
GT2010-22706 The Influence of Cooling Flows on the Operating Conditions of the Ultra-Supercritical Steam Turbine ComponentsKosman, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2237
-
GT2010-22740 Loss Coefficient Dependence of Turbine Blade CascadeMatejka, M. / Safarik, P. / Luxa, M. / Simurda, D. / Synac, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2245
-
GT2010-22747 The Development of Long Last Stage Steam Turbine BladesMcBean, I. / Havakechian, S. / Masserey, P.-A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2257
-
GT2010-22796 Numerical and Experimental Investigations of Unsteady 3-D Wet-steam Flows Through Two-Stage Stator-Rotor Cascade ChannelsYamamoto, S. / Sasao, Y. / Kato, H. / Satsuki, H. / Ooyama, H. / Ishizaka, K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2267
-
GT2010-22807 Unsteady Forces Acting on the Rotor Blade and Shaft in the Control Stage for Different Steam Admission VariantsRomualdwski, R. / Solinski, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2277
-
GT2010-22995 Fatigue Life Extension of Steam Turbine Alloys Using Low Plasticity Burnishing (LPB)Prevey, P.S. / Jayaraman, N. / Ravindranath, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2289
-
GT2010-23021 Numerical Study on the Condensing Flow in Low Pressure Cylinder of a 300MW Steam TurbineLi, L. / Li, Y. / Wu, L. / You, W. / Li, J. / Feng, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2297
-
GT2010-23231 A 150 kW Radial Inflow Steam Turbine System for the Bottoming Cycle of Reciprocating EnginesNakano, S. / Tsubouchi, K. / Shiraiwa, H. / Hayashi, K. / Yamada, H. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2309
-
GT2010-23568 Thermally Sprayed Abradable Coatings in Steam Turbines: Design Integration and Functionality TestingSporer, D. / Wilson, S. / Fiala, P. / Schuelein, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2319
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GT2010-23704 Numerical Study of Internal Flow Fields in Steam Turbine Stages With Balance HolesLuo, C. / Song, L. / Li, J. / Feng, Z. / Cao, S. / Wu, Z. / Wu, Q. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2329
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GT2010-23788 Analysis of Fluid-Structure Interaction in a Steam Turbine Throttle ValveTecza, J. / Chochua, G. / Moll, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2339
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GT2010-22054 Experimental Study of Acoustic Resonances in the Side Cavities of a High-Pressure Centrifugal Compressor Excited by Rotor/Stator InteractionPetry, N. / Koenig, S. / Benra, F.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2353
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GT2010-22104 Unsteady Tip Leakage Flow Characteristics and Heat Transfer on Turbine Blade Tip and CasingRahman, M.H. / Kim, S.I. / Hassan, I. / El Ayoubi, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2363
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GT2010-22269 3D Unsteady Computation of Stall Inception in Axial CompressorsTu, B. / Hu, J. / Zhao, Y. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2373
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GT2010-22276 Numerical Simulation of Flow Instabilities in High Speed Multistage CompressorsZhang, H. / Hu, J. / Tu, B. / Wang, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2383
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GT2010-22284 Stability Enhancement by Casing Grooves: The Importance of Stall Inception Mechanism and SolidityHoughton, T. / Day, I. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2393
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GT2010-22441 Mean Line Flow Model of Steady and Pulsating Flow of a Mixed-Flow Turbine TurbochargerMamat, A.M.I.B. / Martinez-Botas, R.F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2405
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GT2010-22489 Numerical Investigation of the Unsteady Flow Fields in Centrifugal Compressor DiffusersAbdelwahab, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2419
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GT2010-22576 PIV Analysis on the Effect of Stator Loading on Transonic Blade-Row InteractionsReynolds, S.B. / Estevadeordal, J. / Gorrell, S.E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2431
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GT2010-22596 A New Test Rig for Time-Resolved Pressure Measurements in Rotating Cavities With Pulsed InflowSchroeder, G. / Uffrecht, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2441
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GT2010-22762 Unsteady CFD Methods in a Commercial Solver for Turbomachinery ApplicationsBiesinger, T. / Cornelius, C. / Braune, A. / Rube, C. / Campregher, R. / Godin, P.G. / Schmid, G. / Zori, L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2453
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GT2010-22777 Compressor Performance and Operability in Swirl DistortionSheoran, Y. / Bouldin, B. / Krishnan, P.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2465
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GT2010-22845 Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine PerformanceSmith, C.I. / Chang, D. / Tavoularis, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2477
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GT2010-22869 Flow Field in a Single-Stage Model Air Turbine Rotor-Stator Cavity With Pre-Swirled Purge FlowDunn, D.M. / Zhou, D.W. / Squires, K.D. / Saha, K. / Roy, R.P. / Kim, Y.W. / Moon, H.K. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2489
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GT2010-22902 Transient Numerical Investigation of Rotor Clocking in 1.5 Stage of an Axial Test Turbine With a Blade-To-Vane Ratio of 1.5Kusterer, K. / Moritz, N. / Bohn, D. / Sugimoto, T. / Tanaka, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2499
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GT2010-22927 Unsteady Aerodynamics of a Low Aspect Ratio Turbine Stage: Modeling Issues and Flow PhysicsPersico, G. / Mora, A. / Gaetani, P. / Savini, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2511
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GT2010-22977 A CFD and Experimental Investigation of Unsteady Wake Effects on a Highly Loaded Low Pressure Turbine Blade at Low Reynolds NumberSanders, D.D. / Nessler, C.A. / Sondergaard, R. / Polanka, M.D. / Marks, C. / Wolff, M. / O Brien, W.F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2525
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GT2010-23013 Experimental and Numerical Study of Steady and Modulated Transverse Jets at Low Blowing RatiosBidan, G. / Boulladoux, P.-E. / Oertling, J.E. / Nikitopoulos, D.E. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2537
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GT2010-23015 LES Flow Control Simulations for Highly Loaded Low Pressure Turbine Airfoil (L1A) Using Pulsed Vortex Generator JetsIbrahim, M.B. / Kartuzova, O. / Volino, R.J. / Doucet, D.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2553
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GT2010-23024 Numerical Study on Unsteadiness of Tip Clearance Flow Induced by Downstream Stator Row in Axial CompressorHwang, Y. / Kang, S.-H. / Lee, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2561
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GT2010-23025 Flow Structures in the Tip Region for a Transonic Compressor RotorLin, F. / Du, J. / Biela, C. / Chen, J. / Nie, C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2573
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GT2010-23034 Effect of Hot Streak Migration on Unsteady Blade Row Interaction in an Axial TurbineJenny, P. / Lenherr, C. / Kalfas, A. / Abhari, R.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2585
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GT2010-23105 Effects of Bowed Stator on a Fan Characteristic With Distorted InletSun, P. / Zhong, J. / Yang, M. / Han, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2593
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GT2010-23183 Effects of Fan Speed on Rotating Stall Inception and RecoveryChoi, M. / Vahdati, M. / Imregun, M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2605
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GT2010-23297 URANS Predictions of the Effects of Synthetic Jets on the Separated, Transitional Flow Over a Low-Pressure-Turbine-Like Flat PlateMarconcini, M. / Pacciani, R. / Arnone, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2615
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GT2010-23342 Modeling of Surge Characteristics in Turbo Heat PumpsKim, H.R. / Song, S.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2627
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GT2010-23465 Detached Eddy Simulation of Unsteady Stall Flows of a Full Annulus Transonic RotorIm, H.-S. / Chen, X. / Zha, G.-C. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2643
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GT2010-23522 Investigation of Unsteady Flow Effects in an Axial Compressor Based on Whole Annulus ComputationsRober, T. / Kugeler, E. / Weber, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2657
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GT2010-23526 Analysis on the Effect of a Non-Uniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine StagesSalvadori, S. / Montomoli, F. / Martelli, F. / Chana, K.S. / Qureshi, I. / Povey, T. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2671
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GT2010-23541 A Method for Evaluating the Effect of Circumferential Inlet Distortion on the Aerodynamic Stability of Multi-Stage Axial-Flow CompressorsNakano, T. / Breeze-Stringfellow, A. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2685
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GT2010-23567 Separation Control on a Very High Lift Low Pressure Turbine Airfoil Using Pulsed Vortex Generator JetsVolino, R.J. / Kartuzova, O. / Ibrahim, M.B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2701
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GT2010-23573 Effect of Unsteady Wakes on Boundary Layer Separation on a Very High Lift Low Pressure Turbine AirfoilVolino, R.J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2715
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GT2010-23681 Predictions of Unsteady Interactions Between Closely Coupled HP and LP Turbines With Co- and Counter-RotationPraisner, T.J. / Grover, E. / Mocanu, R. / Jurek, R. / Gacek, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2725
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GT2010-23713 Axial Transonic Rotor and Stage Behavior Near the Stability LimitGannon, A.J. / Hobson, G.V. / Davis, W.L. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2735
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GT2010-23755 Hybrid LES/RANS Study of Turbulent Flow in a Linear Compressor Cascade With Moving CasingBorello, D. / Delibra, G. / Hanjalic, K. / Rispoli, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2745
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GT2010-22230 Performance of a Round Ejector With 22.5^o Bent Entraining DiffuserChen, Q. / Birk, A.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2757
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GT2010-22738 Generation of Turbine Maps Using a Fusion of Validated Operational Data and Streamline Curvature MethodZwingenberg, M. / Benra, F.-K. / Werner, K. / Dobrzynski, B. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2769
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GT2010-22933 Towards Investigation of Combustor Turbine Interaction in an Integrated SimulationKlapdor, E.V. / Pyliouras, S. / Eggels, R.L.G.M. / Janicka, J. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2781
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GT2010-23170 Integrated Combustor and Vane Concept in Gas TurbinesRosic, B. / Denton, J.D. / Horlock, J.H. / Uchida, S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2793
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GT2010-23499 Effect of Entraining Diffuser on the Performance of Bent Exhaust EjectorsMaqsood, A. / Birk, A.M. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2803
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GT2010-22014 Diagnosis and Solution of High Noise and Vibration Issues After a Propylene Refrigeration Compressor Re-RateLiu, Z. / Kuzdzal, M.J. / Atkins, K.E. / Rials, R. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2813
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GT2010-22408 Identification of Acoustic Dipole Sources in a Propylene Centrifugal Compressor StageTang, H. / Qi, D. / Lu, F. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2821
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GT2010-22554 Rotor Interaction Noise in Counter-Rotating Propfan Propulsion SystemsPeters, A. / Spakovszky, Z.S. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2835
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GT2010-22696 Modeling of Aerodynamic Noise Using Hybrid SAS and DES MethodsRulik, S. / Dykas, S. / Wroblewski, W. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010
- 2845
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GT2010-23280 Internal Flow and Noise Investigations About the Cross-Flow Fan With Different Blade AnglesLi, Y. / Hua, O. / Jie, T. / Zheng, Z. / Du, Z. / American Society of Mechanical Engineers; ASME International Gas Turbine Institute et al. | 2010