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Issues
October 1989
ISSN 0889-504X
EISSN 1528-8900
In this Issue
Research Papers
Low Aspect Ratio Axial Flow Compressors: Why and What It Means
J. Turbomach. October 1989, 111(4): 357–365.
doi: https://doi.org/10.1115/1.3262280
Topics:
Axial flow
,
Compressors
,
Design
,
Aircraft
,
Design engineering
,
Engines
,
Gas turbines
,
Fans
,
Pendulums
,
Stability
Investigations of Boundary Layer Transition in an Adverse Pressure Gradient
J. Turbomach. October 1989, 111(4): 366–374.
doi: https://doi.org/10.1115/1.3262281
Stability of a Laminar Boundary Layer Flowing Along a Concave Surface
J. Turbomach. October 1989, 111(4): 376–386.
doi: https://doi.org/10.1115/1.3262284
Topics:
Boundary layers
,
Stability
,
Flow (Dynamics)
,
Galerkin method
,
Polynomials
,
Pressure
,
Vortices
,
Waves
Numerical Prediction of Turbine Vane-Blade Aerodynamic Interaction
J. Turbomach. October 1989, 111(4): 387–393.
doi: https://doi.org/10.1115/1.3262285
Topics:
Blades
,
Turbines
,
Airfoils
,
Boundary-value problems
,
Algorithms
,
Inflow
,
Interpolation
,
Outflow
,
Pressure
,
Reflection
A Study of Unsteady Rotor–Stator Interactions
J. Turbomach. October 1989, 111(4): 394–400.
doi: https://doi.org/10.1115/1.3262286
Topics:
Rotors
,
Stators
,
Pressure
,
Wakes
,
Turbulence
,
Oscillations
,
Blades
,
Cylinders
,
Drag (Fluid dynamics)
,
Eddies (Fluid dynamics)
Sensitivity Analysis and Optimum Design Method for Reduced Rotor-Stator-Strut Flow Interaction
J. Turbomach. October 1989, 111(4): 401–408.
doi: https://doi.org/10.1115/1.3262287
Topics:
Design methodology
,
Flow (Dynamics)
,
Rotors
,
Sensitivity analysis
,
Stators
,
Struts (Engineering)
,
Pressure
,
Optimization
,
Performance
,
Wave amplitude
Experimental Investigation of Multistage Interaction Gust Aerodynamics
J. Turbomach. October 1989, 111(4): 409–417.
doi: https://doi.org/10.1115/1.3262288
Topics:
Aerodynamics
,
Airfoils
,
Axial flow
,
Blades
,
Compressors
,
Flow (Dynamics)
,
Flow separation
,
Physics
,
Stators
Experimental Investigation of Rotating Stall in a Mismatched Three-Stage Axial Flow Compressor
J. Turbomach. October 1989, 111(4): 418–425.
doi: https://doi.org/10.1115/1.3262289
Topics:
Axial flow
,
Compressors
,
Stall inception
,
Surges
Application of Bifurcation Theory to Axial Flow Compressor Instability
J. Turbomach. October 1989, 111(4): 426–433.
doi: https://doi.org/10.1115/1.3262290
Topics:
Axial flow
,
Bifurcation
,
Surges
,
Compression
,
Shapes
,
Stress
Numerical Results for Axial Flow Compressor Instability
J. Turbomach. October 1989, 111(4): 434–441.
doi: https://doi.org/10.1115/1.3262291
Topics:
Approximation
,
Axial flow
,
Bifurcation
,
Compressors
,
Emission spectroscopy
,
Flow (Dynamics)
,
Inlet guide vanes
,
Pressure
,
Shapes
,
Spectroscopy
Weak Rotating Flow Disturbances in a Centrifugal Compressor With a Vaneless Diffuser
J. Turbomach. October 1989, 111(4): 442–449.
doi: https://doi.org/10.1115/1.3262292
Topics:
Compressors
,
Flow (Dynamics)
,
Vaneless diffusers
,
Diffusers
,
Resonance
,
Waves
,
Rotation
,
Blades
,
Compression
The Vortex-Filament Nature of Reverse Flow on the Verge of Rotating Stall
J. Turbomach. October 1989, 111(4): 450–461.
doi: https://doi.org/10.1115/1.3262293
Topics:
Flow (Dynamics)
,
Vortices
,
Rotors
,
Clearances (Engineering)
,
Compressors
,
Impellers
,
Boundary layers
,
Leakage flows
,
Rotating bodies
,
Turbulence
Flutter of a Fan Blade in Supersonic Axial Flow
J. Turbomach. October 1989, 111(4): 462–467.
doi: https://doi.org/10.1115/1.3262294
Topics:
Axial flow
,
Blades
,
Flutter (Aerodynamics)
,
Cascades (Fluid dynamics)
,
Compressors
,
Damping
,
Mach number
,
Stress
Turbomachinery Blade Vibration and Dynamic Stress Measurements Utilizing Nonintrusive Techniques
J. Turbomach. October 1989, 111(4): 468–474.
doi: https://doi.org/10.1115/1.3262295
Topics:
Blades
,
Stress
,
Turbomachinery
,
Vibration
,
Failure
,
Acoustics
,
Design
,
Doppler measurement
,
Finite element analysis
,
Fluids
Two-Component Phase-Averaged Turbulence Statistics Downstream of a Rotating Spoked-Wheel Wake Generator
J. Turbomach. October 1989, 111(4): 475–482.
doi: https://doi.org/10.1115/1.3262296
Topics:
Generators
,
Statistics
,
Turbulence
,
Wakes
,
Wheels
,
Stress
,
Vortex shedding
,
Cylinders
,
Density
,
Fluctuations (Physics)
A Quasi-Steady Approach of Wake Effects on Leading Edge Transfer Rates
J. Turbomach. October 1989, 111(4): 483–490.
doi: https://doi.org/10.1115/1.3262297
Topics:
Wakes
,
Mass transfer
,
Turbulence
,
Airfoils
,
Circular cylinders
,
Flow (Dynamics)
,
Gas turbines
The Influence of a Mainstream Thermal Boundary Layer on Film Effectiveness
J. Turbomach. October 1989, 111(4): 491–496.
doi: https://doi.org/10.1115/1.3262298
Topics:
Thermal boundary layers
,
Flow (Dynamics)
,
Heating
,
Geometry
,
Temperature
,
Temperature distribution
,
Wall temperature
The Effect of Free-Stream Turbulence on Gas Turbine Blade Heat Transfer
J. Turbomach. October 1989, 111(4): 497–501.
doi: https://doi.org/10.1115/1.3262299
Correlation and Prediction of Film Cooling From Two Rows of Holes
J. Turbomach. October 1989, 111(4): 502–509.
doi: https://doi.org/10.1115/1.3262300
Topics:
Film cooling
,
Momentum
,
Turbulence
Optimum Trailing Edge Ejection for Cooled Gas Turbine Blades
J. Turbomach. October 1989, 111(4): 510–514.
doi: https://doi.org/10.1115/1.3262301
Topics:
Blades
,
Gas turbines
,
Flow (Dynamics)
,
Cooling
Pressure Loss Distribution in Three-Pass Rectangular Channels With Rib Turbulators
J. Turbomach. October 1989, 111(4): 515–521.
doi: https://doi.org/10.1115/1.3262302
Topics:
Airfoils
,
Cooling
,
Design
,
Flow (Dynamics)
,
Friction
,
Pressure
,
Pressure drop
,
Reynolds number
,
Turbines
Preswirl Blade-Cooling Effectiveness in an Adiabatic Rotor–Stator System
J. Turbomach. October 1989, 111(4): 522–529.
doi: https://doi.org/10.1115/1.3262303
Topics:
Blades
,
Cooling
,
Rotors
,
Stators
,
Temperature
,
Disks
,
Flow (Dynamics)
,
Nozzles
,
Turbines
,
Contamination
A Comparison of Secondary Flow in a Vane Cascade and a Curved Duct
J. Turbomach. October 1989, 111(4): 530–536.
doi: https://doi.org/10.1115/1.3262304
Topics:
Cascades (Fluid dynamics)
,
Ducts
,
Flow (Dynamics)
,
Shapes
,
Aerodynamics
,
Junctions
,
Turbines
,
Vortices
Discussions
Discussion: “Investigations of Boundary Layer Transition in an Adverse Pressure Gradient” (Gostelow, J. P., and Blunden, A. R., 1989, ASME J. Turbomach., 111, pp. 366–374)
J. Turbomach. October 1989, 111(4): 374.
doi: https://doi.org/10.1115/1.3262282
Topics:
Boundary layers
,
Pressure gradient
Closure to “Discussion of ‘Investigations of Boundary Layer Transition in an Adverse Pressure Gradient’” (1989, ASME J. Turbomach., 111, p. 374)
J. Turbomach. October 1989, 111(4): 374–375.
doi: https://doi.org/10.1115/1.3262283
Topics:
Boundary layers
,
Pressure
