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Volume 138, Issue 7
July 2016
Issue Cover
ISSN 0889-504X
EISSN 1528-8900
In this Issue

Research Papers

Experimental Evaluation of Large Spacing Compound Angle Full-Coverage Film Cooling Arrays: Adiabatic Film Cooling Effectiveness
Greg Natsui, Roberto Claretti, Mark A. Ricklick, Jayanta S. Kapat, Michael E. Crawford, Glenn Brown, Kenneth Landis
J. Turbomach. July 2016, 138(7): 071001. doi: https://doi.org/10.1115/1.4032538
View articletitled, Experimental Evaluation of Large Spacing Compound Angle Full-Coverage Film Cooling Arrays: Adiabatic Film Cooling Effectiveness
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Topics: Film cooling , Temperature , Coolants
Full Coverage Shaped-Hole Film Cooling in an Accelerating Boundary Layer With High Freestream Turbulence
J. E. Kingery, F. E. Ames
J. Turbomach. July 2016, 138(7): 071002. doi: https://doi.org/10.1115/1.4031867
View articletitled, Full Coverage Shaped-Hole Film Cooling in an Accelerating Boundary Layer With High Freestream Turbulence
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Topics: Film cooling , Turbulence , Heat transfer
Direct Numerical Simulations of a High-Pressure Turbine Vane
Andrew P. S. Wheeler, Richard D. Sandberg, Neil D. Sandham, Richard Pichler, Vittorio Michelassi, Greg Laskowski
J. Turbomach. July 2016, 138(7): 071003. doi: https://doi.org/10.1115/1.4032435
View articletitled, Direct Numerical Simulations of a High-Pressure Turbine Vane
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Topics: Flow (Dynamics) , Heat transfer , Suction , Turbines , Turbulence , Computer simulation , High pressure (Physics) , Energy dissipation , Boundary layers , Mach number
A New Test Facility to Investigate Film Cooling on a Nonaxisymmetric Contoured Turbine Endwall—Part II: Heat Transfer and Film Cooling Measurements
Johannes Kneer, Franz Puetz, Achmed Schulz, Hans-Jörg Bauer
J. Turbomach. July 2016, 138(7): 071004. doi: https://doi.org/10.1115/1.4032364
View articletitled, A New Test Facility to Investigate Film Cooling on a Nonaxisymmetric Contoured Turbine Endwall—Part II: Heat Transfer and Film Cooling Measurements
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Topics: Film cooling , Heat transfer , Temperature , Turbines , Coolants , Test facilities
Film Cooling Parameter Waveforms on a Turbine Blade Leading Edge Model With Oscillating Stagnation Line
James L. Rutledge, Tylor C. Rathsack, Matthew T. Van Voorhis, Marc D. Polanka
J. Turbomach. July 2016, 138(7): 071005. doi: https://doi.org/10.1115/1.4032455
View articletitled, Film Cooling Parameter Waveforms on a Turbine Blade Leading Edge Model With Oscillating Stagnation Line
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Topics: Coolants , Film cooling , Flow (Dynamics) , Oscillations , Temperature , Heat transfer , Turbine blades , Plumes (Fluid dynamics)
The Delta Phi Method of Evaluating Overall Film Cooling Performance
James L. Rutledge, Marc D. Polanka, David G. Bogard
J. Turbomach. July 2016, 138(7): 071006. doi: https://doi.org/10.1115/1.4032456
View articletitled, The Delta Phi Method of Evaluating Overall Film Cooling Performance
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Topics: Film cooling , Temperature , Cooling
Numerical Investigation of Kelvin–Helmholtz Instability in a Centrifugal Compressor Operating Near Stall
Y. Bousquet, N. Binder, G. Dufour, X. Carbonneau, I. Trebinjac, M. Roumeas
J. Turbomach. July 2016, 138(7): 071007. doi: https://doi.org/10.1115/1.4032457
View articletitled, Numerical Investigation of Kelvin–Helmholtz Instability in a Centrifugal Compressor Operating Near Stall
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Topics: Blades , Compressors , Flow (Dynamics) , Impellers , Momentum , Pressure , Shear (Mechanics) , Diffusers , Vortex shedding
Implicit Large Eddy Simulation of a Stalled Low-Pressure Turbine Airfoil
C. L. Memory, J. P. Chen, J. P. Bons
J. Turbomach. July 2016, 138(7): 071008. doi: https://doi.org/10.1115/1.4032365
View articletitled, Implicit Large Eddy Simulation of a Stalled Low-Pressure Turbine Airfoil
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Topics: Airfoils , Flow (Dynamics) , Pressure , Separation (Technology) , Shear (Mechanics) , Turbines , Wakes , Reynolds number , Vortices , Vorticity
A Novel Mixing Plane Method Using Nonreflecting Boundary Conditions for Multirow Analysis in Turbomachines
Fernando Gisbert, Roque Corral
J. Turbomach. July 2016, 138(7): 071009. doi: https://doi.org/10.1115/1.4032539
View articletitled, A Novel Mixing Plane Method Using Nonreflecting Boundary Conditions for Multirow Analysis in Turbomachines
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Topics: Boundary-value problems , Flow (Dynamics) , Flux (Metallurgy) , Compressors , Turbomachinery , Momentum , Errors
All Issues
Optimization of Low-Pressure Turbine Blade by Means of Fine Inspection of Loss Production Mechanisms
J. Turbomach
Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor
J. Turbomach
Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions
J. Turbomach
CONTROL OF SHROUD LEAKAGE LOSS AND WINDAGE TORQUE IN A LOW-PRESSURE TURBINE STAGE
J. Turbomach
Numerical implementation of electrostatic solver within OpenFOAM for GT intake filtration
J. Turbomach
  • Online ISSN 1528-8900
  • Print ISSN 0889-504X

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