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Proceedings Papers

Proceedings Volume Cover
ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition
June 11–14, 1990
Brussels, Belgium
Conference Sponsors:
  • International Gas Turbine Institute
ISBN:
978-0-7918-7904-7
In This Volume
Volume 1: Turbomachinery

Turbomachinery

Advances in the Numerical Analysis of Linearized Unsteady Cascade Flows
W. J. Usab, Jr., J. M. Verdon
GT 1990; V001T01A002https://doi.org/10.1115/90-GT-011
View Articletitled, Advances in the Numerical Analysis of Linearized Unsteady Cascade Flows
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Topics: Cascades (Fluid dynamics) , Flow (Dynamics) , Numerical analysis , Unsteady flow , Composite materials , Compressors , Blades , Flutter (Aerodynamics) , Mach number , Modeling
Three-Dimensional Rotational Flow in Transonic Turbomachines: Part I — Solution Obtained by Using a Number of S1 Stream Filaments of Revolution and a Central S2 Stream Filament
Wu Chung-Hua, Wang Zhengming, Chen Hongji
GT 1990; V001T01A003https://doi.org/10.1115/90-GT-012
View Articletitled, Three-Dimensional Rotational Flow in Transonic Turbomachines: Part I — Solution Obtained by Using a Number of S<sub>1</sub> Stream Filaments of Revolution and a Central S<sub>2</sub> Stream Filament
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Topics: Rotational flow , Turbomachinery , Flow (Dynamics) , Design , Approximation , Mach number , Rotors , Shock (Mechanics)
Three-Dimensional Rotational Flow in Transonic Turbomachines: Part II — Full 3D Flow in CAS Rotor Obtained by Using a Number of S1 and S2 Stream Filaments
Wu Chung-Hua, Zhao Xiaolu, Qin Lisen
GT 1990; V001T01A004https://doi.org/10.1115/90-GT-013
View Articletitled, Three-Dimensional Rotational Flow in Transonic Turbomachines: Part II — Full 3D Flow in CAS Rotor Obtained by Using a Number of S<sub>1</sub> and S<sub>2</sub> Stream Filaments
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Topics: Flow (Dynamics) , Rotational flow , Rotors , Turbomachinery , Transonic flow , Mach number , Lasers , Shock (Mechanics)
Analysis of Unsteady Compressible Viscous Layers
G. D. Power, J. M. Verdon, K. A. Kousen
GT 1990; V001T01A005https://doi.org/10.1115/90-GT-014
View Articletitled, Analysis of Unsteady Compressible Viscous Layers
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Topics: Algebra , Blades , Boundary layers , Compressible flow , Flat plates , Flow (Dynamics) , Heat transfer , Heating , Rotors , Stators
Inviscid-Viscous Interaction Analysis of Compressor Cascade Performance
M. Barnett, D. E. Hobbs, D. E. Edwards
GT 1990; V001T01A006https://doi.org/10.1115/90-GT-015
View Articletitled, Inviscid-Viscous Interaction Analysis of Compressor Cascade Performance
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Topics: Cascades (Fluid dynamics) , Compressors , Pressure , Wakes , Airfoils , Blades , Boundary layers , Inviscid flow , Modeling , Separation (Technology)
Rotating Cavity With Axial Throughflow of Cooling Air: Flow Structure
P. R. Farthing, C. A. Long, J. M. Owen, J. R. Pincombe
GT 1990; V001T01A007https://doi.org/10.1115/90-GT-017
View Articletitled, Rotating Cavity With Axial Throughflow of Cooling Air: Flow Structure
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Topics: Air flow , Cavities , Cooling , Vortices , Disks , Flow (Dynamics) , Reynolds number , Axial flow , Compressors , Engines
Towards Improved Throughflow Capability: The Use of 3D Viscous Flow Solvers in a Multistage Environment
W. N. Dawes
GT 1990; V001T01A008https://doi.org/10.1115/90-GT-018
View Articletitled, Towards Improved Throughflow Capability: The Use of 3D Viscous Flow Solvers in a Multistage Environment
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Topics: Blades , Compressors , Flow (Dynamics) , Machinery , Nozzle guide vanes , Rotors , Steam turbines , Turbomachinery , Viscous flow
The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines
J. D. Denton
GT 1990; V001T01A009https://doi.org/10.1115/90-GT-019
View Articletitled, The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines
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Topics: Turbomachinery , Viscous flow , Blades , Flow (Dynamics) , Boundary-value problems , Computational methods , Machinery , Unsteady flow
Secondary Flow Measurements in a Turbine Cascade With High Inlet Turbulence
D. G. Gregory-Smith, J. G. E. Cleak
GT 1990; V001T01A010https://doi.org/10.1115/90-GT-020
View Articletitled, Secondary Flow Measurements in a Turbine Cascade With High Inlet Turbulence
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Topics: Cascades (Fluid dynamics) , Flow measurement , Turbines , Turbulence , Flow (Dynamics) , Blades , Stress , Resonance , Shear stress , Spectra (Spectroscopy)
Three-Dimensional Wake Decay Inside of a Compressor Cascade and its Influence on the Downstream Unsteady Flow Field: Part I — Wake Decay Characteristics in the Flow Passage
C. Poensgen, H. E. Gallus
GT 1990; V001T01A011https://doi.org/10.1115/90-GT-021
View Articletitled, Three-Dimensional Wake Decay Inside of a Compressor Cascade and its Influence on the Downstream Unsteady Flow Field: Part I — Wake Decay Characteristics in the Flow Passage
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Topics: Cascades (Fluid dynamics) , Compressors , Flow (Dynamics) , Unsteady flow , Wakes , Rotors , Stators , Turbulence , Blades , Chords (Trusses)
Three-Dimensional Wake Decay Inside of a Compressor Cascade and its Influence on the Downstream Unsteady Flow Field: Part II — Unsteady Flow Field Downstream of the Stator
C. Poensgen, H. E. Gallus
GT 1990; V001T01A012https://doi.org/10.1115/90-GT-022
View Articletitled, Three-Dimensional Wake Decay Inside of a Compressor Cascade and its Influence on the Downstream Unsteady Flow Field: Part II — Unsteady Flow Field Downstream of the Stator
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Topics: Cascades (Fluid dynamics) , Compressors , Stators , Unsteady flow , Wakes , Rotors , Turbulence , Blades , Chords (Trusses) , Cylinders
Study of Internal Flows in a Mixed-Flow Pump Impeller at Various Tip Clearances Using 3D Viscous Flow Computations
Akira Goto
GT 1990; V001T01A013https://doi.org/10.1115/90-GT-036
View Articletitled, Study of Internal Flows in a Mixed-Flow Pump Impeller at Various Tip Clearances Using 3D Viscous Flow Computations
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Topics: Computation , Flow (Dynamics) , Internal flow , Pump impellers , Viscous flow , Wakes , Boundary layers , Leakage flows
Mechanics on the Tip Clearance Loss of Impeller Blades
Yasutoshi Senoo
GT 1990; V001T01A014https://doi.org/10.1115/90-GT-037
View Articletitled, Mechanics on the Tip Clearance Loss of Impeller Blades
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Topics: Blades , Clearances (Engineering) , Impellers , Pressure , Drag (Fluid dynamics) , Flow (Dynamics) , Kinetic energy , Turbomachinery
Mixing in Axial Flow Compressors: Part I — Test Facilities and Measurements in a Four-Stage Compressor
Y. S. Li, N. A. Cumpsty
GT 1990; V001T01A015https://doi.org/10.1115/90-GT-038
View Articletitled, Mixing in Axial Flow Compressors: Part I — Test Facilities and Measurements in a Four-Stage Compressor
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Topics: Axial flow , Compressors , Test facilities , Ducts , Machinery , Stators
Mixing in Axial Flow Compressors: Part II — Measurements in a Single Stage Compressor and a Duct
Y. S. Li, N. A. Cumpsty
GT 1990; V001T01A016https://doi.org/10.1115/90-GT-039
View Articletitled, Mixing in Axial Flow Compressors: Part II — Measurements in a Single Stage Compressor and a Duct
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Topics: Axial flow , Compressors , Ducts , Flow (Dynamics) , Wakes , Blades , Corners (Structural elements) , Inlet guide vanes , Turbulent diffusion , Anisotropy
Experimental Study of the Swirling Flow in the Volute of a Centrifugal Pump
T. Elholm, E. Ayder, R. Van Den Braembussche
GT 1990; V001T01A017https://doi.org/10.1115/90-GT-049
View Articletitled, Experimental Study of the Swirling Flow in the Volute of a Centrifugal Pump
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Topics: Centrifugal pumps , Conservation laws (Physics) , Cross section (Physics) , Design , Flow (Dynamics) , Flow visualization , Fluids , Pipes , Pressure , Pressure drop
Two Dimensional Flow Analysis of a Laboratory Centrifugal Pump
S. M. Miner, R. D. Flack, P. E. Allaire
GT 1990; V001T01A018https://doi.org/10.1115/90-GT-050
View Articletitled, Two Dimensional Flow Analysis of a Laboratory Centrifugal Pump
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Topics: Centrifugal pumps , Flow (Dynamics) , Impellers , Design , Pumps , Finite element analysis , Lasers , Rotation , Steady state , Velocimeters
The Influence of Blade Lean on Turbine Losses
S. Harrison
GT 1990; V001T01A019https://doi.org/10.1115/90-GT-055
View Articletitled, The Influence of Blade Lean on Turbine Losses
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Topics: Blades , Turbines , Cascades (Fluid dynamics) , Boundary layers , Design , Flow (Dynamics) , Suction , Turbine blades
Three-Dimensional Flow in an Axial Turbine: Part 1 — Aerodynamic Mechanisms
David Joslyn, Robert Dring
GT 1990; V001T01A020https://doi.org/10.1115/90-GT-056
View Articletitled, Three-Dimensional Flow in an Axial Turbine: Part 1 — Aerodynamic Mechanisms
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Topics: Flow (Dynamics) , Turbine components , Airfoils , Rotors , Turbines , Flow visualization , Pressure , Stators , Temperature profiles , Yaw
Three-Dimensional Flow in an Axial Turbine: Part 2 — Profile Attenuation
David Joslyn, Robert Dring
GT 1990; V001T01A021https://doi.org/10.1115/90-GT-057
View Articletitled, Three-Dimensional Flow in an Axial Turbine: Part 2 — Profile Attenuation
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Topics: Flow (Dynamics) , Turbine components , Airfoils , Turbines , Rotors , Temperature profiles , Combustion chambers , Stators
Thermogasdynamic Effects of the Engine Turbines With the Contra-Rotating Rotors
Y. V. Sotsenko
GT 1990; V001T01A022https://doi.org/10.1115/90-GT-063
View Articletitled, Thermogasdynamic Effects of the Engine Turbines With the Contra-Rotating Rotors
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Topics: Engines , Rotors , Turbines , Clearances (Engineering) , Deflection , Design , Flow (Dynamics) , Fluids
An Analysis of the Viscous Flow Through a Compact Radial Turbine by the Average Passage Approach
James D. Heidmann, Timothy A. Beach
GT 1990; V001T01A023https://doi.org/10.1115/90-GT-064
View Articletitled, An Analysis of the Viscous Flow Through a Compact Radial Turbine by the Average Passage Approach
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Topics: Turbines , Viscous flow , Blades , Flow (Dynamics) , Clearances (Engineering) , Modeling , Temperature , Computers , Entropy , Physics
Aerodynamic Analysis of a Two Stage Transonic Compressor With Variable Stator Vanes
K.-D. Broichhausen, P. Harster
GT 1990; V001T01A024https://doi.org/10.1115/90-GT-073
View Articletitled, Aerodynamic Analysis of a Two Stage Transonic Compressor With Variable Stator Vanes
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Topics: Compressors , Stators , Rotors , Inlet guide vanes , Shock (Mechanics) , Wakes , Blades , Boundary layer turbulence , Bubbles , Cascades (Fluid dynamics)
The Turbine Regime of a Rear Axial Compressor Stage
Václav Cyrus
GT 1990; V001T01A025https://doi.org/10.1115/90-GT-074
View Articletitled, The Turbine Regime of a Rear Axial Compressor Stage
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Topics: Compressors , Turbines , Flow (Dynamics) , Design , Blades , Pressure , Probes , Rotors , Stators
LDV Measurements of Turbulent Stresses in Radial Turbine Guide Vanes
Hasan Eroglu, Widen Tabakoff
GT 1990; V001T01A026https://doi.org/10.1115/90-GT-075
View Articletitled, LDV Measurements of Turbulent Stresses in Radial Turbine Guide Vanes
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Topics: Guide vanes , Stress , Turbines , Turbulence , Flow (Dynamics) , Anisotropy , Corners (Structural elements) , Cross-flow , Data acquisition systems , Electromagnetic scattering
Viscous Flow Computations in Turbomachine Cascades
P.-A. Chevrin, C. Vuillez
GT 1990; V001T01A027https://doi.org/10.1115/90-GT-076
View Articletitled, Viscous Flow Computations in Turbomachine Cascades
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Topics: Computation , Turbomachinery , Viscous flow , Flow (Dynamics) , Cascades (Fluid dynamics) , Compressors , Turbines , Geometry , Navier-Stokes equations , Turbulence
Viscous Flow Field Calculations in High-Loaded Centrifugal Compressor Diffusers
Ingolf Teipel, Alexander Wiedermann
GT 1990; V001T01A028https://doi.org/10.1115/90-GT-077
View Articletitled, Viscous Flow Field Calculations in High-Loaded Centrifugal Compressor Diffusers
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Topics: Compressors , Diffusers , Viscous flow , Turbulence , Boundary layers , Approximation , Computation , Computers , Eddies (Fluid dynamics) , Modeling
A Study on the Blade Shape Influence on Flow Distribution and Performance in Centrifugal Compressor Rotors
Raffaele Tuccillo, Adolfo Senatore
GT 1990; V001T01A029https://doi.org/10.1115/90-GT-099
View Articletitled, A Study on the Blade Shape Influence on Flow Distribution and Performance in Centrifugal Compressor Rotors
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Topics: Blades , Compressors , Flow (Dynamics) , Rotors , Shapes , Boundary layers , Aircraft engines , Geometry , Momentum , Pressure
Basic Analysis of Counter-Rotating Turbines
R. Cai, W. Wu, G. Fang
GT 1990; V001T01A030https://doi.org/10.1115/90-GT-108
View Articletitled, Basic Analysis of Counter-Rotating Turbines
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Topics: Turbines , Stress , Blades , Design , Engines , Gas turbines , Power stations , Rotating blades
Dynamic Control of Centrifugal Compressor Surge Using Tailored Structures
D. L. Gysling, J. Dugundji, E. M. Greitzer, A. H. Epstein
GT 1990; V001T01A031https://doi.org/10.1115/90-GT-122
View Articletitled, Dynamic Control of Centrifugal Compressor Surge Using Tailored Structures
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Topics: Compressors , Surges , Compression , Dynamics (Mechanics) , Feedback , Flow (Dynamics) , Limit cycles , Linear systems , Oscillations , Pressure
Active Stabilization of Centrifugal Compressor Surge
J. E. Pinsley, G. R. Guenette, A. H. Epstein, E. M. Greitzer
GT 1990; V001T01A032https://doi.org/10.1115/90-GT-123
View Articletitled, Active Stabilization of Centrifugal Compressor Surge
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Topics: Compressors , Surges , Control equipment , Oscillations , Compression , Flow (Dynamics) , Pressure , Valves , Damping , Design
Investigation of the Flow at the Exit of an Unshrouded Centrifugal Impeller and Comparison With the “Classical” Jet-Wake Theory
K.-H. Rohne, M. Banzhaf
GT 1990; V001T01A033https://doi.org/10.1115/90-GT-124
View Articletitled, Investigation of the Flow at the Exit of an Unshrouded Centrifugal Impeller and Comparison With the “Classical” Jet-Wake Theory
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Topics: Flow (Dynamics) , Impellers , Wakes , Blades , Compressors , Shapes
Tip Leakage Flow in Axial Compressors
J. A. Storer, N. A. Cumpsty
GT 1990; V001T01A034https://doi.org/10.1115/90-GT-127
View Articletitled, Tip Leakage Flow in Axial Compressors
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Topics: Compressors , Leakage flows , Blades , Clearances (Engineering) , Flow (Dynamics) , Pressure , Cascades (Fluid dynamics) , Chords (Trusses) , Leakage , Machinery
Centrifugal Compressor Impeller Aerodynamics: An Experimental Investigation
H. David Joslyn, Joost J. Brasz, Robert P. Dring
GT 1990; V001T01A035https://doi.org/10.1115/90-GT-128
View Articletitled, Centrifugal Compressor Impeller Aerodynamics: An Experimental Investigation
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Topics: Aerodynamics , Compressor impellers , Blades , Flow (Dynamics) , Flow visualization , Impellers , Pressure , Compressors
Wake Measurements and Loss Evaluation in a Controlled Diffusion Compressor Cascade
R. P. Shreeve, Y. Elazar, J. W. Dreon, A. Baydar
GT 1990; V001T01A036https://doi.org/10.1115/90-GT-129
View Articletitled, Wake Measurements and Loss Evaluation in a Controlled Diffusion Compressor Cascade
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Topics: Cascades (Fluid dynamics) , Compressors , Diffusion (Physics) , Wakes , Blades , Pressure , Design , Probes , Chords (Trusses) , Flow (Dynamics)
Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels
J. P. Gostelow, G. J. Walker
GT 1990; V001T01A037https://doi.org/10.1115/90-GT-130
View Articletitled, Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels
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Topics: Boundary layers , Pressure gradient , Turbulence , Equilibrium (Physics) , Boundary layer turbulence , Shear stress , Skin friction (Fluid dynamics)
The Effects of Wake Mixing on Compressor Aerodynamics
Robert P. Dring, David A. Spear
GT 1990; V001T01A039https://doi.org/10.1115/90-GT-132
View Articletitled, The Effects of Wake Mixing on Compressor Aerodynamics
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Topics: Aerodynamics , Compressors , Wakes , Airfoils , Flow (Dynamics) , Corners (Structural elements) , Pressure , Separation (Technology)
Unsteady Radial Transport in a Transonic Compressor Stage
P. A. Kotidis, A. H. Epstein
GT 1990; V001T01A040https://doi.org/10.1115/90-GT-133
View Articletitled, Unsteady Radial Transport in a Transonic Compressor Stage
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Topics: Compressors , Rotors , Wakes , Fluids , Blades , Entropy , Pressure , Temperature , Vortex street , Frequency response
Pressure Losses in Combining Subsonic Flows Through Branched Ducts
N. I. Abou-Haidar, S. L. Dixon
GT 1990; V001T01A041https://doi.org/10.1115/90-GT-134
View Articletitled, Pressure Losses in Combining Subsonic Flows Through Branched Ducts
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Topics: Ducts , Pressure , Subsonic flow , Flow (Dynamics) , Junctions , Flow separation , Flow visualization , Fluids , Mach number , Schlieren methods
Computation of Heat Transfer in Rotating Cavities Using a Two-Equation Model of Turbulence
A. P. Morse, C. L. Ong
GT 1990; V001T01A042https://doi.org/10.1115/90-GT-135
View Articletitled, Computation of Heat Transfer in Rotating Cavities Using a Two-Equation Model of Turbulence
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Topics: Cavities , Computation , Heat transfer , Turbulence , Disks , Reynolds number , Convection , Cooling , Engineering design , Errors
A Numerical Study of the Influence of Disc Geometry on the Flow and Heat Transfer in a Rotating Cavity
B. L. Lapworth, J. W. Chew
GT 1990; V001T01A043https://doi.org/10.1115/90-GT-136
View Articletitled, A Numerical Study of the Influence of Disc Geometry on the Flow and Heat Transfer in a Rotating Cavity
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Topics: Cavities , Disks , Flow (Dynamics) , Geometry , Heat transfer , Turbulence , Boundary-value problems , Navier-Stokes equations , Outflow
Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application
W. Steinert, B. Eisenberg, H. Starken
GT 1990; V001T01A044https://doi.org/10.1115/90-GT-140
View Articletitled, Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application
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Topics: Airfoils , Axial flow , Cascades (Fluid dynamics) , Design , Diffusion (Physics) , Testing , Compressors , Blades , Boundary layers , Computational methods
Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade
A. Yamamoto, Y. Kondo, R. Murao
GT 1990; V001T01A045https://doi.org/10.1115/90-GT-141
View Articletitled, Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade
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Topics: Cascades (Fluid dynamics) , Cooling , Flow (Dynamics) , Turbines , Blades , Internal flow , Kinetic energy , Turbine blades , Vortices
Impeller Flow Field Measurement and Analysis
John Robert Fagan, Sanford Fleeter
GT 1990; V001T01A046https://doi.org/10.1115/90-GT-146
View Articletitled, Impeller Flow Field Measurement and Analysis
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Topics: Flow (Dynamics) , Impellers , Compressors , Internal flow , Wakes , Design , Pressure , Suction
Compressor Drum Aerodynamic Experiments and Analysis With Coolant Injected at Selected Locations
B. V. Johnson, W. A. Daniels, E. J. Kawecki, R. J. Martin
GT 1990; V001T01A047https://doi.org/10.1115/90-GT-151
View Articletitled, Compressor Drum Aerodynamic Experiments and Analysis With Coolant Injected at Selected Locations
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Topics: Compressors , Coolants , Flow (Dynamics) , Cavities , Disks , Pressure , Viscosity , Aircraft engines , Boundary layers , High pressure (Physics)
The Development of Axial Turbine Leakage Loss for Two Profiled Tip Geometries Using Linear Cascade Data
Jeffrey P. Bindon, George Morphis
GT 1990; V001T01A048https://doi.org/10.1115/90-GT-152
View Articletitled, The Development of Axial Turbine Leakage Loss for Two Profiled Tip Geometries Using Linear Cascade Data
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Topics: Cascades (Fluid dynamics) , Leakage , Turbines , Blades , Bubbles , Clearances (Engineering) , Separation (Technology) , Rotors , Discharge coefficient , Flow (Dynamics)
Similarity Analysis of Compressor Tip Clearance Flow Structure
G. T. Chen, E. M. Greitzer, C. S. Tan, F. E. Marble
GT 1990; V001T01A049https://doi.org/10.1115/90-GT-153
View Articletitled, Similarity Analysis of Compressor Tip Clearance Flow Structure
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Topics: Clearances (Engineering) , Compressors , Flow (Dynamics) , Cross-flow , Vortices , Pressure gradient , Trajectories (Physics) , Aerodynamics , Approximation , Blades
Prediction of Tip-Leakage Losses in Axial Turbines
M. I. Yaras, S. A. Sjolander
GT 1990; V001T01A050https://doi.org/10.1115/90-GT-154
View Articletitled, Prediction of Tip-Leakage Losses in Axial Turbines
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Topics: Leakage , Turbines , Flow (Dynamics) , Physics , Turbomachinery
Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row
H. E. Gallus, C. Hah, H. D. Schulz
GT 1990; V001T01A051https://doi.org/10.1115/90-GT-155
View Articletitled, Experimental and Numerical Investigation of Three-Dimensional Viscous Flows and Vortex Motion Inside an Annular Compressor Blade Row
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Topics: Blades , Compressors , Flow (Dynamics) , Vortex motion , Boundary layers , Cascades (Fluid dynamics) , Corners (Structural elements) , Flow visualization , Navier-Stokes equations , Numerical analysis
Rotating Waves as a Stall Inception Indication in Axial Compressors
V. H. Garnier, A. H. Epstein, E. M. Greitzer
GT 1990; V001T01A052https://doi.org/10.1115/90-GT-156
View Articletitled, Rotating Waves as a Stall Inception Indication in Axial Compressors
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Topics: Compressors , Stall inception , Waves , Machinery , Inflow
Passive Control of Unstable Characteristics of a High Specific Speed Diagonal-Flow Fan by an Annular Wing
Kenji Kaneko, Toshiaki Setoguchi, Masahiro Inoue
GT 1990; V001T01A055https://doi.org/10.1115/90-GT-159
View Articletitled, Passive Control of Unstable Characteristics of a High Specific Speed Diagonal-Flow Fan by an Annular Wing
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Topics: Flow (Dynamics) , Passive control , Wings , Airfoils , Design , Internal flow , Nozzles , Pressure , Testing performance
Essential Ingredients for the Computation of Steady and Unsteady Blade Boundary Layers
H. M. Jang, M. F. Platzer, J. A. Ekaterinaris, T. Cebeci
GT 1990; V001T01A056https://doi.org/10.1115/90-GT-160
View Articletitled, Essential Ingredients for the Computation of Steady and Unsteady Blade Boundary Layers
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Topics: Blades , Boundary layers , Computation , Flow (Dynamics) , Reynolds number , Airfoils , Inviscid flow , Navier-Stokes equations , Pressure , Viscous flow
Secondary Flow and Loss Distribution in a Radial Compressor With Untwisted Backswept Vanes
G. Sipos
GT 1990; V001T01A057https://doi.org/10.1115/90-GT-161
View Articletitled, Secondary Flow and Loss Distribution in a Radial Compressor With Untwisted Backswept Vanes
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Topics: Compressors , Flow (Dynamics) , Impellers , Blades , Separation (Technology) , Vortices , Suction , Wakes , Whirls , Diffusers
A Contribution to Designing a Radial Flow Gas Turbine Stage
F. S. Bhinder
GT 1990; V001T01A058https://doi.org/10.1115/90-GT-187
View Articletitled, A Contribution to Designing a Radial Flow Gas Turbine Stage
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Topics: Design , Gas turbines , Radial flow , Rotors , Equilibrium (Physics) , Flow (Dynamics) , Momentum , Nozzles
A Fully Compressible Three Dimensional Inverse Design Method Applicable to Radial and Mixed Flow Turbomachines
M. Zangeneh, W. R. Hawthrone
GT 1990; V001T01A059https://doi.org/10.1115/90-GT-198
View Articletitled, A Fully Compressible Three Dimensional Inverse Design Method Applicable to Radial and Mixed Flow Turbomachines
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Topics: Design methodology , Flow (Dynamics) , Turbomachinery , Blades , Density , Impellers , Shapes , Algorithms , Compressible flow , Design
An Experimental Investigation of Loss Reduction With Riblets on Cascade Blade Surfaces and Isolated Airfoils
Chen Fang, Tang Yan-Ping, Chen Mao-Zhang
GT 1990; V001T01A060https://doi.org/10.1115/90-GT-207
View Articletitled, An Experimental Investigation of Loss Reduction With Riblets on Cascade Blade Surfaces and Isolated Airfoils
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Topics: Airfoils , Blades , Cascades (Fluid dynamics) , Compressors , Pressure , Drag reduction , Suction
Effects of Surface Roughness, Freestream Turbulence, and Incidence Angle on the Performance of a 2-D Compressor Cascade
W. C. Elrod, P. I. King, E. M. Poniatowski
GT 1990; V001T01A061https://doi.org/10.1115/90-GT-208
View Articletitled, Effects of Surface Roughness, Freestream Turbulence, and Incidence Angle on the Performance of a 2-D Compressor Cascade
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Topics: Cascades (Fluid dynamics) , Compressors , Surface roughness , Turbulence , Blades , Airfoils , Chords (Trusses) , Flow (Dynamics) , Pressure , Suction
The Interaction Between the Axial Compressor and the Downstream Distorting Component
Guo-Cai Tang
GT 1990; V001T01A062https://doi.org/10.1115/90-GT-209
View Articletitled, The Interaction Between the Axial Compressor and the Downstream Distorting Component
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Topics: Compressors , Flow (Dynamics) , Aircraft , Blades , Compressible flow , Gas turbines , Pressure
An Investigation of the Dynamic Characteristic of Axial Flow Compressors
Guo-Cai Tang, Bing Hu, Hui-Ming Zhang
GT 1990; V001T01A063https://doi.org/10.1115/90-GT-210
View Articletitled, An Investigation of the Dynamic Characteristic of Axial Flow Compressors
PDF
Topics: Axial flow , Compressors , Steady state , Valves , Flow (Dynamics) , Algebra , Transients (Dynamics)
Basic Features of Speed Induced Transient Behaviour of Axial Flow Compressors
G. C. Tang
GT 1990; V001T01A064https://doi.org/10.1115/90-GT-211
View Articletitled, Basic Features of Speed Induced Transient Behaviour of Axial Flow Compressors
PDF
Topics: Axial flow , Compressors , Transients (Dynamics) , Flow (Dynamics) , Surges , Compression
Flowfield Calculation in Compressor Operating With Distorted Inlet Flow
H. Joubert
GT 1990; V001T01A065https://doi.org/10.1115/90-GT-212
View Articletitled, Flowfield Calculation in Compressor Operating With Distorted Inlet Flow
PDF
Topics: Compressors , Flow (Dynamics) , Blades , Actuators , Chords (Trusses) , Disks , Engines , Pressure , Resolution (Optics) , Stability
Centrifugal Compressor Impeller Aerodynamics: A Numerical Investigation
Daniel J. Dorney, Roger L. Davis
GT 1990; V001T01A066https://doi.org/10.1115/90-GT-213
View Articletitled, Centrifugal Compressor Impeller Aerodynamics: A Numerical Investigation
PDF
Topics: Aerodynamics , Compressor impellers , Blades , Flow (Dynamics) , Impellers , Design , Equations of motion , Partial differential equations , Rotors , Stators
Measured and Predicted Effects of Inlet Distortion on Axial Compressors
J. P. Longley
GT 1990; V001T01A067https://doi.org/10.1115/90-GT-214
View Articletitled, Measured and Predicted Effects of Inlet Distortion on Axial Compressors
PDF
Topics: Compressors , Fluid dynamics , Inlet guide vanes , Modeling
Inlet Flow Distortion Effects on Rotating Stall
J. Fortin, W. C. Moffatt
GT 1990; V001T01A068https://doi.org/10.1115/90-GT-215
View Articletitled, Inlet Flow Distortion Effects on Rotating Stall
PDF
Topics: Flow (Dynamics) , Compressors , Surges , Fluctuations (Physics) , Probes , Rotors , Cycles , Damping , Engines , Jet engines
Experimental Investigation of the Stalled Flow in a Centrifugal Pump-Turbine With Varied Diffuser
Marina Ubaldi, Pietro Zunino
GT 1990; V001T01A069https://doi.org/10.1115/90-GT-216
View Articletitled, Experimental Investigation of the Stalled Flow in a Centrifugal Pump-Turbine With Varied Diffuser
PDF
Topics: Diffusers , Flow (Dynamics) , Pump turbines , Pressure , Impellers , Pumps , Fourier transforms , Probes , Signals , Wire
A Boundary Layer Transition Correlation for Concave Surfaces
Farouk Hachem, Mark W. Johnson
GT 1990; V001T01A070https://doi.org/10.1115/90-GT-222
View Articletitled, A Boundary Layer Transition Correlation for Concave Surfaces
PDF
Topics: Boundary layers , Momentum , Blades , Reynolds number , Turbulence , Vortices , Flat plates , Shapes
Aerothermal Boundary Layer Computation Including Strong Viscous-Inviscid Flow Interaction
P. Kulisa, F. Leboeuf, P. Klinger, J. Bernard
GT 1990; V001T01A071https://doi.org/10.1115/90-GT-223
View Articletitled, Aerothermal Boundary Layer Computation Including Strong Viscous-Inviscid Flow Interaction
PDF
Topics: Boundary layers , Computation , Flow (Dynamics) , Turbine blades , Cooling , Heat transfer , Pressure gradient , Advanced materials , Aircraft engines , Bubbles
An Engine Demonstration of Active Surge Control
J. E. Ffowcs Williams, W. R. Graham
GT 1990; V001T01A072https://doi.org/10.1115/90-GT-224
View Articletitled, An Engine Demonstration of Active Surge Control
PDF
Topics: Engines , Surges , Compression , Control systems , Gas turbines , Noise (Sound) , Signals , Stability , Turbochargers
Numerical Prediction of Film Cooling Effectiveness and the Associated Aerodynamic Losses With a Three-Dimensional Calculation Procedure
G. H. Dibelius, R. Pitt, B. Wen
GT 1990; V001T01A073https://doi.org/10.1115/90-GT-226
View Articletitled, Numerical Prediction of Film Cooling Effectiveness and the Associated Aerodynamic Losses With a Three-Dimensional Calculation Procedure
PDF
Topics: Film cooling , Flow (Dynamics) , Cooling , Momentum , Temperature , Boundary-value problems , Computer simulation , Service life (Equipment) , Turbine blades
Prediction of the Aerodynamic and Thermal Environment in Turbines
Lisa W. Griffin, Kelly A. Belford
GT 1990; V001T01A074https://doi.org/10.1115/90-GT-227
View Articletitled, Prediction of the Aerodynamic and Thermal Environment in Turbines
PDF
Topics: Turbines , Cascades (Fluid dynamics) , Airfoils , Boundary layers , Flow (Dynamics) , Computation , Heat transfer , Pressure , Stators , Viscous flow
Vortex Control Over End Wall Flow in Compressor Cascades
Yan-Ping Tang, Mao-Zhang Chen
GT 1990; V001T01A075https://doi.org/10.1115/90-GT-228
View Articletitled, Vortex Control Over End Wall Flow in Compressor Cascades
PDF
Topics: Compressors , Flow (Dynamics) , Vortices , Cascades (Fluid dynamics) , Physics , Pressure
Energy Exchange and Secondary Losses Prediction in High Speed Axial and Radial Compressors
J. K. Kaldellis, P. D. Ktenidis, D. E. Kodossakis
GT 1990; V001T01A076https://doi.org/10.1115/90-GT-229
View Articletitled, Energy Exchange and Secondary Losses Prediction in High Speed Axial and Radial Compressors
PDF
Topics: Compressors , Machinery , Flow (Dynamics) , Cascades (Fluid dynamics) , Computational methods , Fluids , Shear (Mechanics) , Vorticity
An Interactive System to Integrate the Design, Analysis, and Manufacture of Centrifugal Compressor Impellers
James E. Crouse, James M. Sorokes
GT 1990; V001T01A077https://doi.org/10.1115/90-GT-230
View Articletitled, An Interactive System to Integrate the Design, Analysis, and Manufacture of Centrifugal Compressor Impellers
PDF
Topics: Compressor impellers , Design , Computer software , Engineering drawing and drafting , Impellers , Manufacturing , Polynomials
The Effect of Backswept Blading on the Flow in a Centrifugal Compressor Impeller
Talib Z. Farge, Mark W. Johnson
GT 1990; V001T01A078https://doi.org/10.1115/90-GT-231
View Articletitled, The Effect of Backswept Blading on the Flow in a Centrifugal Compressor Impeller
PDF
Topics: Compressor impellers , Flow (Dynamics) , Impellers , Blades , Boundary layers , Separation (Technology) , Vortices , Wakes
Unsteady Velocity- and Turbulence Measurements With a Fast Response Pressure Probe
G. Ruck, H. Stetter
GT 1990; V001T01A079https://doi.org/10.1115/90-GT-232
View Articletitled, Unsteady Velocity- and Turbulence Measurements With a Fast Response Pressure Probe
PDF
Topics: Pressure , Probes , Turbulence , Compressors , Damage , Flow (Dynamics) , Pressure transducers , Risk , Rotating blades , Rotors
Flow Investigation in a Small High Speed Impeller Passage Using Laser Anemometry
N. A. Ahmed, R. L. Elder
GT 1990; V001T01A080https://doi.org/10.1115/90-GT-233
View Articletitled, Flow Investigation in a Small High Speed Impeller Passage Using Laser Anemometry
PDF
Topics: Flow (Dynamics) , Impellers , Lasers , Laser velocimetry , Wakes
A Prediction of 3-D Viscous Flow and Performance of the NASA Low-Speed Centrifugal Compressor
John Moore, Joan G. Moore
GT 1990; V001T01A081https://doi.org/10.1115/90-GT-234
View Articletitled, A Prediction of 3-D Viscous Flow and Performance of the NASA Low-Speed Centrifugal Compressor
PDF
Topics: Compressors , NASA , Viscous flow , Flow (Dynamics) , Impellers , Design , Leakage flows , Clearances (Engineering) , Compressor impellers , Flow measurement
Three Dimensional Design of a High Speed Radial-Inflow Turbine by a Novel Design Method
M. Zangeneh
GT 1990; V001T01A082https://doi.org/10.1115/90-GT-235
View Articletitled, Three Dimensional Design of a High Speed Radial-Inflow Turbine by a Novel Design Method
PDF
Topics: Design , Design methodology , Inflow , Turbines , Impellers , Blades , Shapes , Casting , Diesel engines , Turbochargers
Boundary Layer and Navier-Stokes Analysis of a NASA Controlled-Diffusion Compressor Blade
Y. K. Ho, G. J. Walker, P. Stow
GT 1990; V001T01A083https://doi.org/10.1115/90-GT-236
View Articletitled, Boundary Layer and Navier-Stokes Analysis of a NASA Controlled-Diffusion Compressor Blade
PDF
Topics: Blades , Boundary layers , Compressors , Diffusion (Physics) , NASA , Design , Modeling , Boundary layer turbulence , Bubbles , Computational methods
Semi-Inverse Design of Compressor Cascades, Including Supersonic Inflow
A. Kirschner, H. Stoff
GT 1990; V001T01A084https://doi.org/10.1115/90-GT-237
View Articletitled, Semi-Inverse Design of Compressor Cascades, Including Supersonic Inflow
PDF
Topics: Compressors , Design , Inflow , Blades , Flow (Dynamics) , Geometry , Cascades (Fluid dynamics) , Design methodology , Turbomachinery
Developments Leading to an Axial Flow Compressor for a 25 MW Class High Efficiency Gas Turbine
Y. Kashiwabara, Y. Katoh, H. Ishii, T. Hattori, Y. Matsuura, T. Sasada
GT 1990; V001T01A085https://doi.org/10.1115/90-GT-238
View Articletitled, Developments Leading to an Axial Flow Compressor for a 25 MW Class High Efficiency Gas Turbine
PDF
Topics: Axial flow , Gas turbines , Compressors , Design , Design engineering , Pressure , Steady state , Surges , Unsteady flow
Influence of Periodically Unsteady Wake Flow on the Flow Separation in Blade Channels
G. H. Dibelius, E. Ahlers
GT 1990; V001T01A086https://doi.org/10.1115/90-GT-253
View Articletitled, Influence of Periodically Unsteady Wake Flow on the Flow Separation in Blade Channels
PDF
Topics: Blades , Flow separation , Wakes , Flow (Dynamics) , Turbulence , Boundary layers , Flat plates , Pressure , Suction , Turbine blades
Laser Velocimeter Measurements in a Centrifugal Pump With a Synchronously Orbiting Impeller
Ronald J. Beaudoin, Steven M. Miner, Ronald D. Flack
GT 1990; V001T01A087https://doi.org/10.1115/90-GT-258
View Articletitled, Laser Velocimeter Measurements in a Centrifugal Pump With a Synchronously Orbiting Impeller
PDF
Topics: Centrifugal pumps , Impellers , Lasers , Velocimeters , Blades , Flow (Dynamics) , Design , Pumps , Flux (Metallurgy) , Momentum
Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part 1 — Experiment
R. Charles Stauter, Robert P. Dring, Franklin O. Carta
GT 1990; V001T01A088https://doi.org/10.1115/90-GT-259
View Articletitled, Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part 1 — Experiment
PDF
Topics: Compressors , Flow (Dynamics) , Rotors , Fluid dynamics , Stators , Turbomachinery , Aerodynamics , Fluids , Probes , Resolution (Optics)
A Zonal Approach for Navier-Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method
M. Furukawa, M. Yamasaki, M. Inoue
GT 1990; V001T01A089https://doi.org/10.1115/90-GT-260
View Articletitled, A Zonal Approach for Navier-Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method
PDF
Topics: Computation , Finite volume methods , Flow (Dynamics) , Flux (Metallurgy) , Cascades (Fluid dynamics) , Composite materials , Mesh generation , Navier-Stokes equations , Turbines
Prediction of Cascade Performance Using an Incompressible Navier-Stokes Technique
G. V. Hobson, B. Lakshminarayana
GT 1990; V001T01A090https://doi.org/10.1115/90-GT-261
View Articletitled, Prediction of Cascade Performance Using an Incompressible Navier-Stokes Technique
PDF
Topics: Cascades (Fluid dynamics) , Pressure , Turbulence , Blades , Boundary layers , Compressors , Momentum , Navier-Stokes equations , Poisson equation , Skin friction (Fluid dynamics)
Inviscid and Viscous Solutions for Airfoil/Cascade Flows Using a Locally Implicit Algorithm on Adaptive Meshes
C. J. Hwang, J. L. Liu
GT 1990; V001T01A091https://doi.org/10.1115/90-GT-262
View Articletitled, Inviscid and Viscous Solutions for Airfoil/Cascade Flows Using a Locally Implicit Algorithm on Adaptive Meshes
PDF
Topics: Airfoils , Algorithms , Cascades (Fluid dynamics) , Flow (Dynamics) , Boundary layers , Compressors , Flat plates , Inviscid flow , Laminar flow , Mesh generation
Detailed Boundary Layer Measurements on a Transonic Turbine Cascade
D. J. Mee, N. C. Baines, M. L. G. Oldfield
GT 1990; V001T01A092https://doi.org/10.1115/90-GT-263
View Articletitled, Detailed Boundary Layer Measurements on a Transonic Turbine Cascade
PDF
Topics: Boundary layers , Cascades (Fluid dynamics) , Turbines , Chords (Trusses) , Engines , Pressure , Suction , Thin films , Turbine blades , Turbulence
A Comparison of Zero and One Equation Turbulence Modelling for Turbomachinery Calculations
W. N. Dawes
GT 1990; V001T01A093https://doi.org/10.1115/90-GT-303
View Articletitled, A Comparison of Zero and One Equation Turbulence Modelling for Turbomachinery Calculations
PDF
Topics: Modeling , Turbomachinery , Turbulence , Blades , Compressors , Crude oil , Flow (Dynamics) , Standard model (Physics) , Turbines
Dawes and Denton Codes Applied to a Transonic Compressor Rotor
T. W. Von Backström
GT 1990; V001T01A094https://doi.org/10.1115/90-GT-304
View Articletitled, Dawes and Denton Codes Applied to a Transonic Compressor Rotor
PDF
Topics: Compressors , Rotors , Shock (Mechanics) , Boundary layers , Design , Pressure , Clearances (Engineering) , Flow (Dynamics) , Suction
Nozzle Guide Vane Shock Wave Propagation and Bifurcation in a Transonic Turbine Rotor
A. B. Johnson, M. L. G. Oldfield, M. J. Rigby, M. B. Giles
GT 1990; V001T01A095https://doi.org/10.1115/90-GT-310
View Articletitled, Nozzle Guide Vane Shock Wave Propagation and Bifurcation in a Transonic Turbine Rotor
PDF
Topics: Bifurcation , Nozzle guide vanes , Rotors , Shock waves , Turbines , Bubbles , Pressure , Blades , Heat , Heat transfer
Numerical Prediction of Turbine Profile Loss
L. Xu, J. D. Denton
GT 1990; V001T01A096https://doi.org/10.1115/90-GT-311
View Articletitled, Numerical Prediction of Turbine Profile Loss
PDF
Topics: Blades , Boundary layers , Flow (Dynamics) , Friction , Momentum , Numerical analysis , Pressure , Transonic flow , Turbine blades , Turbines
Overtip Pressure Measurements in a Cold-Flow Turbine Rig
R. C. Kingcombe, I. M. Smith, R. V. Steeden
GT 1990; V001T01A097https://doi.org/10.1115/90-GT-312
View Articletitled, Overtip Pressure Measurements in a Cold-Flow Turbine Rig
PDF
Topics: Flow (Dynamics) , Pressure measurement , Turbines , Rotors , Blades , Frequency response , Pressure transducers
Experimental Analysis Data on the Transonic Flow Past a Plane Turbine Cascade
M. Šťastný, P. Šafařík
GT 1990; V001T01A098https://doi.org/10.1115/90-GT-313
View Articletitled, Experimental Analysis Data on the Transonic Flow Past a Plane Turbine Cascade
PDF
Topics: Cascades (Fluid dynamics) , Experimental analysis , Transonic flow , Turbines , Flow (Dynamics) , Compression , Data collection , Dimensions , Mach number , Rotors
Off-Design Performance of a Linear Cascade of Turbine Blades
B. Tremblay, S. A. Sjolander, S. H. Moustapha
GT 1990; V001T01A099https://doi.org/10.1115/90-GT-314
View Articletitled, Off-Design Performance of a Linear Cascade of Turbine Blades
PDF
Topics: Cascades (Fluid dynamics) , Design , Turbine blades , Pressure , Reynolds number , Airfoils , Blades , Flow visualization , Turbines , Turning angles
High Turning Limit and Jet Like Profiles in Secondary Flow Field of Axial Turbines
J. K. Kaldellis, P. D. Ktenidis
GT 1990; V001T01A100https://doi.org/10.1115/90-GT-327
View Articletitled, High Turning Limit and Jet Like Profiles in Secondary Flow Field of Axial Turbines
PDF
Topics: Flow (Dynamics) , Turbines , Turning , Approximation , Computational methods , Computers , Deflection , Navier-Stokes equations , Viscous flow , Vorticity
Mixing in Axial-Flow Compressors: Conclusions Drawn From 3-D Navier-Stokes Analyses and Experiments
J. H. Leylek, D. C. Wisler
GT 1990; V001T01A101https://doi.org/10.1115/90-GT-352
View Articletitled, Mixing in Axial-Flow Compressors: Conclusions Drawn From 3-D Navier-Stokes Analyses and Experiments
PDF
Topics: Axial flow , Compressors , Flow (Dynamics) , Computation , Design , Stators , Boundary-value problems , Modeling , Numerical analysis , Physics
The Aerodynamic and Mechanical Performance of a High Pressure Turbine Stage in a Transient Wind Tunnel
A. G. Sheard, R. W. Ainsworth
GT 1990; V001T01A102https://doi.org/10.1115/90-GT-353
View Articletitled, The Aerodynamic and Mechanical Performance of a High Pressure Turbine Stage in a Transient Wind Tunnel
PDF
Topics: Equipment performance , High pressure (Physics) , Transients (Dynamics) , Turbines , Wind tunnels , Stress , Aerodynamics , Bearings , Data acquisition , Design
High Speed Compressor Surge With Application to Active Control
A. M. Cargill, C. Freeman
GT 1990; V001T01A103https://doi.org/10.1115/90-GT-354
View Articletitled, High Speed Compressor Surge With Application to Active Control
PDF
Topics: Compressors , Surges , Transducers , Waves , Actuators , Aircraft engines , Stability
Endwall Losses and Flow Unsteadiness in a Turbine Blade Cascade
L. Adjlout, S. L. Dixon
GT 1990; V001T01A104https://doi.org/10.1115/90-GT-355
View Articletitled, Endwall Losses and Flow Unsteadiness in a Turbine Blade Cascade
PDF
Topics: Cascades (Fluid dynamics) , Flow (Dynamics) , Turbine blades , Pressure , Turbulence , Blades , Boundary layers , Flow visualization , Vortices , Oscillations
An Experimental Study of Local Wall Shear Stress, Surface Static Pressure and Flow Visualization Upstream, Alongside, and Downstream of a Blade Endwall Corner
A. K. Abdulla, R. K. Bhargava, R. Raj
GT 1990; V001T01A105https://doi.org/10.1115/90-GT-356
View Articletitled, An Experimental Study of Local Wall Shear Stress, Surface Static Pressure and Flow Visualization Upstream, Alongside, and Downstream of a Blade Endwall Corner
PDF
Topics: Blades , Corners (Structural elements) , Flow visualization , Pressure , Shear stress , Chords (Trusses) , Flow (Dynamics) , Pressure gradient , Vortices
Aero-Thermal Performance of a Two Dimensional Highly Loaded Transonic Turbine Nozzle Guide Vane: A Test Case for Inviscid and Viscous Flow Computations
Tony Arts, Muriel Lambert De Rouvroit
GT 1990; V001T01A106https://doi.org/10.1115/90-GT-358
View Articletitled, Aero-Thermal Performance of a Two Dimensional Highly Loaded Transonic Turbine Nozzle Guide Vane: A Test Case for Inviscid and Viscous Flow Computations
PDF
Topics: Computation , Nozzle guide vanes , Turbines , Viscous flow , Blades , Flow (Dynamics) , Convection , Reynolds number , Turbulence , Aircraft engines
Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades
C. Hah, A. J. Wennerstrom
GT 1990; V001T01A107https://doi.org/10.1115/90-GT-359
View Articletitled, Three-Dimensional Flowfields Inside a Transonic Compressor With Swept Blades
PDF
Topics: Blades , Compressors , Rotors , Flow (Dynamics) , Shock (Mechanics) , Turbulence , Clearances (Engineering) , Modeling , Navier-Stokes equations , Relaxation (Physics)
Comparison of Inviscid Computations With Theory and Experiment in Vibrating Transonic Compressor Cascades
G. A. Gerolymos, E. Blin, H. Quiniou
GT 1990; V001T01A108https://doi.org/10.1115/90-GT-373
View Articletitled, Comparison of Inviscid Computations With Theory and Experiment in Vibrating Transonic Compressor Cascades
PDF
Topics: Compressors , Computation , Blades , Boundary layers , Shock waves , Acoustics , Boundary-value problems , Computational methods , Fans , Flat plates
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