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October 1974
This article was originally published in
Journal of Engineering for Power
ISSN 0022-0825
In this Issue
Research Papers
Heat Transfer and Film Cooling Following Normal Injection Through a Round Hole
J. Eng. Power. October 1974, 96(4): 329–334.
doi: https://doi.org/10.1115/1.3445854
Topics:
Film cooling
,
Heat transfer
,
Heat transfer coefficients
,
Heat flux
,
Turbulence
,
Air jets
,
Boundary layers
,
Flat plates
,
Flow (Dynamics)
,
Jets
Torsional Stability Analysis of a Gas-Turbine Powered Helicopter Drive System
J. Eng. Power. October 1974, 96(4): 335–341.
doi: https://doi.org/10.1115/1.3445855
Topics:
Gas turbines
,
Stability
,
Rotors
,
Trains
,
Design
,
Dynamic systems
,
Engines
,
Excitation
,
Frequency response
,
Governors
Highlights and Future Development of Closed-Cycle Gas Turbines
J. Eng. Power. October 1974, 96(4): 342–348.
doi: https://doi.org/10.1115/1.3445856
Topics:
Closed-cycle gas turbines
,
Design
,
Construction
,
Helium
,
Central heating
,
Coolers
,
Energy consumption
,
Gas turbines
,
Hearths
,
High temperature
Residual Stresses in Gas Turbine Engine Components From Barkhausen Noise Analysis
J. Eng. Power. October 1974, 96(4): 349–357.
doi: https://doi.org/10.1115/1.3445857
Topics:
Gas turbines
,
Noise (Sound)
,
Residual stresses
,
Compressors
,
Stress
,
Ball bearings
,
Blades
,
Calibration
,
Diffusers
,
Disks
Similarity Parameters for Comparing Erosive Particle Trajectories in Hot Air and Cold Air Radial Inflow Turbines
J. Eng. Power. October 1974, 96(4): 358–364.
doi: https://doi.org/10.1115/1.3445858
Topics:
Inflow
,
Particulate matter
,
Turbines
,
Reynolds number
,
Equations of motion
,
Flow (Dynamics)
,
Gas flow
,
Rotors
,
Vortices
A Three-Dimensional Theory for Calculating Circulation in Axial Turbomachines (Direct Problems)
J. Eng. Power. October 1974, 96(4): 365–371.
doi: https://doi.org/10.1115/1.3445859
Topics:
Approximation
,
Blades
,
Cascades (Fluid dynamics)
,
Chords (Trusses)
,
Clearances (Engineering)
,
Errors
,
Steady state
,
Turbomachinery
Lift and Moment Prediction For an Oscillating Airfoil With a Moving Separation Point
J. Eng. Power. October 1974, 96(4): 372–378.
doi: https://doi.org/10.1115/1.3445860
Topics:
Airfoils
,
Separation (Technology)
,
Flat plates
,
Flutter (Aerodynamics)
,
Oscillations
Supersonic Unstalled Flutter In Fan Rotors; Analytical and Experimental Results
J. Eng. Power. October 1974, 96(4): 379–386.
doi: https://doi.org/10.1115/1.3445861
Topics:
Flutter (Aerodynamics)
,
Rotors
,
Cascades (Fluid dynamics)
,
Blades
,
Shapes
,
Wind tunnels
,
Airfoils
,
Flat plates
,
Mach number
,
Testing
Premixed Combustion in a Baffle Combustor and the Effect of Steam Injection
J. Eng. Power. October 1974, 96(4): 387–393.
doi: https://doi.org/10.1115/1.3445862
Topics:
Combustion
,
Combustion chambers
,
Steam
,
Ceramics
,
Pollution
,
Temperature
The M.I.T. Blowdown Compressor Facility
J. Eng. Power. October 1974, 96(4): 394–405.
doi: https://doi.org/10.1115/1.3445863
Topics:
Compressors
,
Rotors
,
Flow (Dynamics)
,
Wakes
,
Pressure
,
Steady state
,
Blades
,
Design
,
Diaphragms (Mechanical devices)
,
Diaphragms (Structural)
Calculation of Cascade Profiles From the Velocity Distribution
J. Eng. Power. October 1974, 96(4): 407–412.
doi: https://doi.org/10.1115/1.3445866
Topics:
Cascades (Fluid dynamics)
,
Computers
,
Flow (Dynamics)
,
Mach number
,
Subsonic flow
End-Wall Boundary Layers in Axial Compressors
J. Eng. Power. October 1974, 96(4): 413–426.
doi: https://doi.org/10.1115/1.3445867
Topics:
Boundary layers
,
Compressors
,
Blades
,
Flow (Dynamics)
,
Shapes
,
Skin friction (Fluid dynamics)
,
Reynolds number
,
Rotors
,
Wood products
Operational Limits for Gas Turbine Compressors During Transient Conditions in a Helium Cooled Reactor
J. Eng. Power. October 1974, 96(4): 427–434.
doi: https://doi.org/10.1115/1.3445871
Topics:
Compressors
,
Gas turbines
,
Helium
,
Transients (Dynamics)
,
Pipes
,
Pressure
,
Rupture
,
Accidents
,
Containment
,
Coolants
Ensuring Stable Circuit Conditions of Direct Cycle Helium Gas Turbine System
J. Eng. Power. October 1974, 96(4): 435–439.
doi: https://doi.org/10.1115/1.3445872
Topics:
Circuits
,
Cycles
,
Gas turbines
,
Helium
,
Compressors
,
Control systems
,
Safety
,
Stress
,
Design
,
Failure
A Generalized Discharge Coefficient for Differential Pressure Type Fluid Meters
J. Eng. Power. October 1974, 96(4): 440–448.
doi: https://doi.org/10.1115/1.3445873
Topics:
Discharge coefficient
,
Flowmeters
,
Pressure
,
Calibration
,
Nozzles
,
Pipes
,
Reynolds number
Discussions
Discussion: “The M.I.T. Blowdown Compressor Facility” (Kerrebrock, J. L., Epstein, A. H., Haines, D. M., and Thompkins, W. T., 1974, ASME J. Eng. Power, 96, pp. 394–405)
J. Eng. Power. October 1974, 96(4): 406.
doi: https://doi.org/10.1115/1.3445864
Topics:
Compressors
Closure to “Discussion of ‘The M.I.T. Blowdown Compressor Facility’” (1974, ASME J. Eng. Power, 96, p. 406)
J. Eng. Power. October 1974, 96(4): 406.
doi: https://doi.org/10.1115/1.3445865
Topics:
Compressors
Discussion: “End-Wall Boundary Layers in Axial Compressors” (Hirsch, Ch., 1974, ASME J. Eng. Power, 96, pp. 413–426)
J. Eng. Power. October 1974, 96(4): 426.
doi: https://doi.org/10.1115/1.3445868
Topics:
Boundary layers
,
Compressors
Closure to “Discussion of ‘End-Wall Boundary Layers in Axial Compressors’” (1974, ASME J. Eng. Power, 96, p. 426)
J. Eng. Power. October 1974, 96(4): 426.
doi: https://doi.org/10.1115/1.3445870
Topics:
Boundary layers
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