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Volume 140, Issue 10
October 2018
Issue Cover
ISSN 0889-504X
EISSN 1528-8900
In this Issue

Research Papers

Condensation in Radial Turbines—Part I: Mathematical Modeling
Sebastian Schuster, Dieter Brillert, Friedrich-Karl Benra
J. Turbomach. October 2018, 140(10): 101001. doi: https://doi.org/10.1115/1.4040934
View articletitled, Condensation in Radial Turbines—Part I: Mathematical Modeling
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Topics: Drops , Flow (Dynamics) , Turbines , Liquid films , Condensation
Condensation in Radial Turbines—Part II: Application of the Mathematical Model to a Radial Turbine Series
Sebastian Schuster, Dieter Brillert, Friedrich-Karl Benra
J. Turbomach. October 2018, 140(10): 101002. doi: https://doi.org/10.1115/1.4040935
View articletitled, Condensation in Radial Turbines—Part II: Application of the Mathematical Model to a Radial Turbine Series
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Topics: Condensation , Drops , Impellers , Subcooling , Turbines , Flow (Dynamics) , Liquid films , Pressure , Blades
The Effect of Nonequilibrium Boundary Layers on Compressor Performance
Andrew P. S. Wheeler, Anthony M. J. Dickens, Robert J. Miller
J. Turbomach. October 2018, 140(10): 101003. doi: https://doi.org/10.1115/1.4040094
View articletitled, The Effect of Nonequilibrium Boundary Layers on Compressor Performance
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Topics: Boundary layers , Compressors , Flow (Dynamics) , Reynolds number , Shear (Mechanics) , Simulation , Suction , Turbulence , Energy dissipation , Blades
Influence of Blade Loading Profile on Wake Dynamics in High-Pressure Turbine Cascades
Benjamin T. Luymes, Qiang An, Adam M. Steinberg, Xuefeng Zhang, Thomas Vandeputte
J. Turbomach. October 2018, 140(10): 101004. doi: https://doi.org/10.1115/1.4041141
View articletitled, Influence of Blade Loading Profile on Wake Dynamics in High-Pressure Turbine Cascades
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Topics: Blades , Wakes , Convection
Numerical Study of Deterministic Fluxes in Compressor Passages
Feng Wang, Mauro Carnevale, Luca di Mare
J. Turbomach. October 2018, 140(10): 101005. doi: https://doi.org/10.1115/1.4041450
View articletitled, Numerical Study of Deterministic Fluxes in Compressor Passages
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Topics: Blades , Compressors , Flow (Dynamics) , Flux (Metallurgy) , Pressure , Simulation , Reynolds-averaged Navier–Stokes equations , Computational fluid dynamics , Ducts , Wakes
Effects of Downstream Vane Bowing and Asymmetry on Unsteadiness in a Transonic Turbine
John P. Clark, Richard J. Anthony, Michael K. Ooten, John M. Finnegan, P. Dean Johnson, Ron-Ho Ni
J. Turbomach. October 2018, 140(10): 101006. doi: https://doi.org/10.1115/1.4040998
View articletitled, Effects of Downstream Vane Bowing and Asymmetry on Unsteadiness in a Transonic Turbine
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Topics: Airfoils , Blades , Design , Pressure , Shock (Mechanics) , Suction , Turbines , Simulation
Effects of Density and Blowing Ratios on the Turbulent Structure and Effectiveness of Film Cooling
Zachary T. Stratton, Tom I-P. Shih
J. Turbomach. October 2018, 140(10): 101007. doi: https://doi.org/10.1115/1.4041218
View articletitled, Effects of Density and Blowing Ratios on the Turbulent Structure and Effectiveness of Film Cooling
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Topics: Boundary layer turbulence , Boundary layers , Density , Film cooling , Flow (Dynamics) , Turbulence , Vortices , Cooling , Shear (Mechanics) , Vorticity
Applying Machine Learnt Explicit Algebraic Stress and Scalar Flux Models to a Fundamental Trailing Edge Slot
R. D. Sandberg, R. Tan, J. Weatheritt, A. Ooi, A. Haghiri, V. Michelassi, G. Laskowski
J. Turbomach. October 2018, 140(10): 101008. doi: https://doi.org/10.1115/1.4041268
View articletitled, Applying Machine Learnt Explicit Algebraic Stress and Scalar Flux Models to a Fundamental Trailing Edge Slot
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Topics: Anisotropy , Heat flux , Large eddy simulation , Reynolds-averaged Navier–Stokes equations , Scalars , Stress , Tensors , Turbulence , Eddies (Fluid dynamics) , Algebra
All Issues
Design Guidelines for Inertial Particle Separators
J. Turbomach
Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
J. Turbomach (October 2025)
An unsteady deposition model for evaluating CMAS nonuniform deposition behavior and aerodynamic performance degradation under hot streak clocking effect
J. Turbomach
HIGH SPEED ROTATING HPT BLADE THERMAL IMAGING OF A FULL SCALE COOLED 1+1/2 STAGE TURBINE IN A SHORT DURATION TRANSIENT TEST FACILITY
J. Turbomach
2024 Associate Editors
J. Turbomach
  • Online ISSN 1528-8900
  • Print ISSN 0889-504X

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