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Issues
October 1991
ISSN 0889-504X
EISSN 1528-8900
In this Issue
Research Papers
The 1991 IGTI Scholar Lecture: The Role of Laminar-Turbulent Transition in Gas Turbine Engines
J. Turbomach. October 1991, 113(4): 509–536.
doi: https://doi.org/10.1115/1.2929110
Inviscid-Viscous Interaction Analysis of Compressor Cascade Performance
J. Turbomach. October 1991, 113(4): 538–552.
doi: https://doi.org/10.1115/1.2929113
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Pressure
,
Wakes
,
Airfoils
,
Blades
,
Boundary layers
,
Inviscid flow
,
Modeling
,
Separation (Technology)
Inviscid and Viscous Solutions for Airfoil/Cascade Flows Using a Locally Implicit Algorithm on Adaptive Meshes
J. Turbomach. October 1991, 113(4): 553–560.
doi: https://doi.org/10.1115/1.2929114
Topics:
Airfoils
,
Algorithms
,
Cascades (Fluid dynamics)
,
Flow (Dynamics)
,
Boundary layers
,
Compressors
,
Flat plates
,
Inviscid flow
,
Laminar flow
,
Mesh generation
Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique
J. Turbomach. October 1991, 113(4): 561–571.
doi: https://doi.org/10.1115/1.2929115
A Zonal Approach for Navier–Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method
J. Turbomach. October 1991, 113(4): 573–582.
doi: https://doi.org/10.1115/1.2929118
Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application
J. Turbomach. October 1991, 113(4): 583–590.
doi: https://doi.org/10.1115/1.2929119
Topics:
Airfoils
,
Axial flow
,
Cascades (Fluid dynamics)
,
Design
,
Diffusion (Physics)
,
Testing
,
Compressors
,
Blades
,
Boundary layers
,
Computational methods
Wake Measurements and Loss Evaluation in a Controlled Diffusion Compressor Cascade
J. Turbomach. October 1991, 113(4): 591–599.
doi: https://doi.org/10.1115/1.2929120
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Diffusion (Physics)
,
Wakes
,
Blades
,
Pressure
,
Design
,
Probes
,
Chords (Trusses)
,
Flow (Dynamics)
The Effects of Wake Mixing on Compressor Aerodynamics
J. Turbomach. October 1991, 113(4): 600–607.
doi: https://doi.org/10.1115/1.2929121
Topics:
Aerodynamics
,
Compressors
,
Wakes
,
Airfoils
,
Flow (Dynamics)
,
Corners (Structural elements)
,
Pressure
,
Separation (Technology)
Essential Ingredients for the Computation of Steady and Unsteady Blade Boundary Layers
J. Turbomach. October 1991, 113(4): 608–616.
doi: https://doi.org/10.1115/1.2929124
Topics:
Blades
,
Boundary layers
,
Computation
,
Flow (Dynamics)
,
Reynolds number
,
Airfoils
,
Inviscid flow
,
Navier-Stokes equations
,
Pressure
,
Viscous flow
Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels
J. Turbomach. October 1991, 113(4): 617–624.
doi: https://doi.org/10.1115/1.2929125
An Experimental Study of Local Wall Shear Stress, Surface Static Pressure, and Flow Visualization Upstream, Alongside, and Downstream of a Blade Endwall Corner
J. Turbomach. October 1991, 113(4): 626–632.
doi: https://doi.org/10.1115/1.2929128
Advances in the Numerical Analysis of Linearized Unsteady Cascade Flows
J. Turbomach. October 1991, 113(4): 633–643.
doi: https://doi.org/10.1115/1.2929129
Analysis of Unsteady Compressible Viscous Layers
J. Turbomach. October 1991, 113(4): 644–653.
doi: https://doi.org/10.1115/1.2929130
Topics:
Algebra
,
Blades
,
Boundary layers
,
Compressible flow
,
Flat plates
,
Flow (Dynamics)
,
Heat transfer
,
Heating
,
Rotors
,
Stators
Investigation of the Flow at the Exit of an Unshrouded Centrifugal Impeller and Comparison With the “Classical” Jet-Wake Theory
J. Turbomach. October 1991, 113(4): 654–659.
doi: https://doi.org/10.1115/1.2929131
Topics:
Flow (Dynamics)
,
Impellers
,
Wakes
,
Blades
,
Compressors
,
Shapes
Centrifugal Compressor Impeller Aerodynamics: An Experimental Investigation
J. Turbomach. October 1991, 113(4): 660–669.
doi: https://doi.org/10.1115/1.2929132
Topics:
Aerodynamics
,
Compressor impellers
,
Blades
,
Flow (Dynamics)
,
Flow visualization
,
Pressure
,
Compressors
,
Impellers
Impeller Flow Field Measurement and Analysis
J. Turbomach. October 1991, 113(4): 670–679.
doi: https://doi.org/10.1115/1.2929133
Topics:
Flow (Dynamics)
,
Impellers
,
Compressors
,
Internal flow
,
Wakes
,
Design
,
Pressure
,
Suction
Mechanics on the Tip Clearance Loss of Impeller Blades
J. Turbomach. October 1991, 113(4): 680–685.
doi: https://doi.org/10.1115/1.2929134
Topics:
Blades
,
Clearances (Engineering)
,
Impellers
,
Pressure
,
Drag (Fluid dynamics)
,
Flow (Dynamics)
,
Kinetic energy
,
Turbomachinery
Secondary Flow and Loss Distribution in a Radial Compressor With Untwisted Backswept Vanes
J. Turbomach. October 1991, 113(4): 686–695.
doi: https://doi.org/10.1115/1.2929135
Topics:
Compressors
,
Flow (Dynamics)
,
Impellers
,
Blades
,
Separation (Technology)
,
Vortices
,
Suction
,
Wakes
,
Whirls
,
Diffusers
Centrifugal Compressor Inlet Guide Vanes for Increased Surge Margin
J. Turbomach. October 1991, 113(4): 696–702.
doi: https://doi.org/10.1115/1.2929136
Topics:
Compressors
,
Inlet guide vanes
,
Surges
,
Diffusers
,
Impellers
,
Stability
,
Compression
,
Mach number
,
Testing
Passive Control of Unstable Characteristics of a High Specific Speed Diagonal-Flow Fan by an Annular Wing
J. Turbomach. October 1991, 113(4): 703–709.
doi: https://doi.org/10.1115/1.2929137
Topics:
Flow (Dynamics)
,
Passive control
,
Wings
,
Airfoils
,
Design
,
Internal flow
,
Nozzles
,
Pressure
,
Testing performance
Dynamic Control of Centrifugal Compressor Surge Using Tailored Structures
J. Turbomach. October 1991, 113(4): 710–722.
doi: https://doi.org/10.1115/1.2929138
Topics:
Compressors
,
Surges
,
Compression
,
Dynamics (Mechanics)
,
Feedback
,
Flow (Dynamics)
,
Limit cycles
,
Linear systems
,
Oscillations
,
Pressure
Active Stabilization of Centrifugal Compressor Surge
J. Turbomach. October 1991, 113(4): 723–732.
doi: https://doi.org/10.1115/1.2929139
Topics:
Compressors
,
Surges
,
Control equipment
,
Oscillations
,
Compression
,
Flow (Dynamics)
,
Pressure
,
Valves
,
Damping
,
Design
Discussions
Discussion: “The Role of Laminar-Turbulent Transition in Gas Turbine Engines” (Mayle, Robert Edward, 1991, ASME J. Turbomach., 113, pp. 509–536)
J. Turbomach. October 1991, 113(4): 536–537.
doi: https://doi.org/10.1115/1.2929111
Topics:
Gas turbines
,
Turbulence
Closure to “Discussion of ‘The Role of Laminar-Turbulent Transition in Gas Turbine Engines’” (1991, ASME J. Turbomach., 113, pp. 536–537)
J. Turbomach. October 1991, 113(4): 537.
doi: https://doi.org/10.1115/1.2929112
Topics:
Gas turbines
,
Turbulence
Discussion: “Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique” (Hobson, G. V., and Lakshminarayana, B., 1991, ASME J. Turbomach., 113, pp. 561–571)
J. Turbomach. October 1991, 113(4): 571–572.
doi: https://doi.org/10.1115/1.2929116
Topics:
Cascades (Fluid dynamics)
Closure to “Discussion of ‘Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique’” (1991, ASME J. Turbomach., 113, pp. 571–572)
J. Turbomach. October 1991, 113(4): 572.
doi: https://doi.org/10.1115/1.2929117
Topics:
Cascades (Fluid dynamics)
Discussion: “The Effects of Wake Mixing on Compressor Aerodynamics” (Dring, R. P., and Spear, D. A., 1991, ASME J. Turbomach., 113, pp. 600–607)
J. Turbomach. October 1991, 113(4): 607.
doi: https://doi.org/10.1115/1.2929122
Topics:
Aerodynamics
,
Compressors
,
Wakes
Closure to “Discussion of ‘The Effects of Wake Mixing on Compressor Aerodynamics’” (1991, ASME J. Turbomach., 113, p. 607)
J. Turbomach. October 1991, 113(4): 607.
doi: https://doi.org/10.1115/1.2929123
Topics:
Compressors
,
Wakes
Discussion: “Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels” (Gostelow, J. P., and Walker, G. J., 1991, ASME J. Turbomach., 113, pp. 617–624)
J. Turbomach. October 1991, 113(4): 624.
doi: https://doi.org/10.1115/1.2929126
Topics:
Boundary layers
,
Pressure gradient
,
Turbulence
Closure to “Discussion of ‘Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels’” (1991, ASME J. Turbomach., 113, p. 624)
J. Turbomach. October 1991, 113(4): 624–625.
doi: https://doi.org/10.1115/1.2929127
Topics:
Boundary layers
,
Pressure gradient
,
Turbulence