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Issues
April 1990
ISSN 0889-504X
EISSN 1528-8900
In this Issue
Research Papers
Design and Testing of the FT8 Gas Turbine Low-Pressure Compressor
J. Turbomach. April 1990, 112(2): 159–164.
doi: https://doi.org/10.1115/1.2927628
Topics:
Compressors
,
Design
,
Gas turbines
,
Pressure
,
Testing
,
Aircraft engines
,
Durability
,
Generators
A Variable-Geometry Power Turbine for Marine Gas Turbines
J. Turbomach. April 1990, 112(2): 165–174.
doi: https://doi.org/10.1115/1.2927629
Topics:
Geometry
,
Marine gas turbines
,
Turbines
,
Engines
,
Nozzles
,
Gas turbines
,
Fuel consumption
,
Propulsion
,
Stress
,
Design
Surface Roughness Measurements on Gas Turbine Blades
J. Turbomach. April 1990, 112(2): 175–180.
doi: https://doi.org/10.1115/1.2927630
Topics:
Blades
,
Gas turbines
,
Surface roughness
,
Turbine blades
,
Boundary layers
,
Computation
,
Engines
,
Flow (Dynamics)
,
Heat transfer
,
Pressure
The Influence of Boundary Layer State on Vortex Shedding From Flat Plates and Turbine Cascades
J. Turbomach. April 1990, 112(2): 181–187.
doi: https://doi.org/10.1115/1.2927631
Topics:
Boundary layers
,
Flat plates
,
Turbines
,
Vortex shedding
,
Blades
,
Turbine blades
,
Cascades (Fluid dynamics)
,
Geometry
,
Mach number
,
Reynolds number
A Theory for Wake-Induced Transition
J. Turbomach. April 1990, 112(2): 188–195.
doi: https://doi.org/10.1115/1.2927632
Topics:
Airfoils
,
Boundary layers
,
Flat plates
,
Heat transfer
,
Turbulence
,
Wake turbulence
,
Wakes
Effects of Adverse Pressure Gradients on the Nature and Length of Boundary Layer Transition
J. Turbomach. April 1990, 112(2): 196–205.
doi: https://doi.org/10.1115/1.2927633
Topics:
Boundary layers
,
Pressure gradient
,
Waves
,
Flow (Dynamics)
,
Reynolds number
,
Separation (Technology)
,
Turbulence
Unsteady Transition in an Axial-Flow Turbine: Part 1—Measurements on the Turbine Rotor
J. Turbomach. April 1990, 112(2): 206–214.
doi: https://doi.org/10.1115/1.2927634
Topics:
Axial flow
,
Rotors
,
Turbine components
,
Turbines
,
Boundary layers
,
Suction
,
Cascades (Fluid dynamics)
,
Cross section (Physics)
,
Gages
,
Stators
Unsteady Transition in an Axial-Flow Turbine: Part 2—Cascade Measurements and Modeling
J. Turbomach. April 1990, 112(2): 215–221.
doi: https://doi.org/10.1115/1.2927635
Topics:
Axial flow
,
Cascades (Fluid dynamics)
,
Modeling
,
Turbine components
,
Turbines
,
Rotors
,
Suction
,
Turbulence
,
Wakes
Compressor Blade Boundary Layers: Part 1—Test Facility and Measurements With No Incident Wakes
J. Turbomach. April 1990, 112(2): 222–230.
doi: https://doi.org/10.1115/1.2927636
Topics:
Blades
,
Boundary layers
,
Compressors
,
Test facilities
,
Wakes
,
Convection
Compressor Blade Boundary Layers: Part 2—Measurements With Incident Wakes
J. Turbomach. April 1990, 112(2): 231–240.
doi: https://doi.org/10.1115/1.2927637
Topics:
Blades
,
Boundary layers
,
Compressors
,
Wakes
,
Momentum
,
Test facilities
,
Turbulence
The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees
J. Turbomach. April 1990, 112(2): 241–255.
doi: https://doi.org/10.1115/1.2927638
Topics:
Blades
,
Boundary layers
,
Cascades (Fluid dynamics)
,
Compressors
,
Flow (Dynamics)
,
Bubbles
,
Pressure
,
Separation (Technology)
,
Chords (Trusses)
,
Turbulence
Viscous Flow in a Controlled Diffusion Compressor Cascade With Increasing Incidence
J. Turbomach. April 1990, 112(2): 256–265.
doi: https://doi.org/10.1115/1.2927642
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Diffusion (Physics)
,
Viscous flow
,
Boundary layers
,
Blades
,
Bubbles
,
Design
,
Flow (Dynamics)
,
Geometry
An Improved Incidence Losses Prediction Method for Turbine Airfoils
J. Turbomach. April 1990, 112(2): 267–276.
doi: https://doi.org/10.1115/1.2927647
The Trailing Edge Loss of Transonic Turbine Blades
J. Turbomach. April 1990, 112(2): 277–285.
doi: https://doi.org/10.1115/1.2927648
Topics:
Turbine blades
,
Pressure
,
Suction
,
Coolants
,
Flow (Dynamics)
,
Momentum
,
Blades
,
Boundary layers
,
Mach number
,
Shock (Mechanics)
An Experimental Assessment of the Influence of Downstream Conditions on the Performance of a Transonic Turbine Nozzle of High Turning
J. Turbomach. April 1990, 112(2): 286–293.
doi: https://doi.org/10.1115/1.2927651
Topics:
Nozzles
,
Turbines
,
Turning
,
Rotors
,
Flow (Dynamics)
,
Design
,
Mach number
,
Pressure
,
Probes
,
Turning angles
The Use of Circumferentially Varying Stagger Guide Vanes in an Axial Flow Pump or Compressor
J. Turbomach. April 1990, 112(2): 294–297.
doi: https://doi.org/10.1115/1.2927652
Topics:
Axial flow
,
Compressors
,
Guide vanes
,
Pumps
,
Pressure
,
Rotors
,
Actuators
,
Disks
,
Flow (Dynamics)
Inlet Distortion Generated Periodic Aerodynamic Rotor Response
J. Turbomach. April 1990, 112(2): 298–307.
doi: https://doi.org/10.1115/1.2927654
Topics:
Rotors
,
Pressure
,
Blades
,
Suction
,
Aerodynamics
,
Axial flow
,
Compressors
,
Design
,
Flow (Dynamics)
Discussions
Discussion: “The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees” (Zierke, W. C., and Deutsch, S., 1990, ASME J. Turbomach., 112, pp. 241–255)
J. Turbomach. April 1990, 112(2): 255.
doi: https://doi.org/10.1115/1.2927639
Topics:
Blades
,
Boundary layers
,
Cascades (Fluid dynamics)
,
Compressors
,
Flow (Dynamics)
Closure to “Discussion of ‘The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees’” (1990, ASME J. Turbomach., 112, p. 255)
J. Turbomach. April 1990, 112(2): 255.
doi: https://doi.org/10.1115/1.2927641
Topics:
Blades
,
Boundary layers
,
Cascades (Fluid dynamics)
,
Compressors
,
Flow (Dynamics)
Discussion: “Viscous Flow in a Controlled Diffusion Compressor Cascade With Increasing Incidence” (Elazar, Y., and Shreeve, R. P., 1990, ASME J. Turbomach., 112, pp. 256–265)
J. Turbomach. April 1990, 112(2): 266.
doi: https://doi.org/10.1115/1.2927644
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Diffusion (Physics)
,
Viscous flow
Closure to “Discussion of ‘Viscous Flow in a Controlled Diffusion Compressor Cascade With Increasing Incidence’” (1990, ASME J. Turbomach., 112, p. 266)
J. Turbomach. April 1990, 112(2): 266.
doi: https://doi.org/10.1115/1.2927645
Topics:
Cascades (Fluid dynamics)
,
Compressors
,
Diffusion (Physics)
,
Viscous flow
Technical Briefs
Visualization Studies in Rotating Disk Cavity Flows
J. Turbomach. April 1990, 112(2): 308–310.
doi: https://doi.org/10.1115/1.2927656
Topics:
Boundary layers
,
Cavities
,
Cavity flows
,
Cooling
,
Disks
,
Flat plates
,
Flow (Dynamics)
,
Flow visualization
,
Particle spin
,
Reynolds number
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