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October 1973
This article was originally published in
Journal of Engineering for Power
ISSN 0022-0825
In this Issue
Research Papers
Review of Compressible Flow Theories for Airfoil Cascades
J. Eng. Power. October 1973, 95(4): 281–292.
doi: https://doi.org/10.1115/1.3445734
Topics:
Airfoils
,
Cascades (Fluid dynamics)
,
Compressible flow
,
Design
,
Flow (Dynamics)
,
Subsonic flow
,
Supersonic flow
Effect of Rotor Design Tip Speed on Aerodynamic Performance of a Model VTOL Lift Fan Under Static and Crossflow Conditions
J. Eng. Power. October 1973, 95(4): 293–300.
doi: https://doi.org/10.1115/1.3445735
Reduction of Nitrogen Oxide Emissions From a Gas Turbine Combustor by Fuel Modifications
J. Eng. Power. October 1973, 95(4): 301–308.
doi: https://doi.org/10.1115/1.3445736
Topics:
Combustion chambers
,
Emissions
,
Fuels
,
Gas turbines
,
Nitrogen oxides
,
Aircraft
,
Pressure
,
Atoms
,
Carbon
,
Catalysts
Calculation of Temperature Distribution in Multistage Axial Gas Turbine Rotor Assemblies When Blades Are Uncooled
J. Eng. Power. October 1973, 95(4): 309–318.
doi: https://doi.org/10.1115/1.3445737
Topics:
Blades
,
Gas turbines
,
Rotor assembly
,
Temperature distribution
,
Disks
,
Rotors
,
Turbines
,
Boundary-value problems
,
Engines
,
Heat transfer
Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate
J. Eng. Power. October 1973, 95(4): 319–325.
doi: https://doi.org/10.1115/1.3445738
Topics:
Flat plates
,
Heat transfer
,
Temperature
,
Boundary layers
,
Enthalpy
,
Heat conduction
,
Turbulent heat transfer
Investigation of the Aerodynamic Performance of Small Axial Turbines
J. Eng. Power. October 1973, 95(4): 326–332.
doi: https://doi.org/10.1115/1.3445739
Topics:
Turbines
,
Blades
,
Design
,
Air flow
,
Airfoils
,
Clearances (Engineering)
,
Cooling
,
Disks
,
Performance characterization
,
Pressure
Evaluation of Additives for Prevention of High Temperature Corrosion of Superalloys in Gas Turbines
J. Eng. Power. October 1973, 95(4): 333–339.
doi: https://doi.org/10.1115/1.3445740
Topics:
Corrosion
,
Gas turbines
,
High temperature
,
Superalloys
,
Fuels
,
Alloys
,
Sodium
,
X-ray diffraction
Numerical Representation of Inlet and Exit Boundary Conditions in Transient Cascade Flow
J. Eng. Power. October 1973, 95(4): 340–344.
doi: https://doi.org/10.1115/1.3445741
Calculation of Compressible Subsonic Flow in Cascades With Varying Blade Height
J. Eng. Power. October 1973, 95(4): 345–351.
doi: https://doi.org/10.1115/1.3445742
Topics:
Blades
,
Subsonic flow
,
Flow (Dynamics)
,
Compressible flow
,
Compressors
,
Density
,
Machinery
,
Pressure
,
Rotational flow
,
Theorems (Mathematics)
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