Volume 108 Issue 2 | J. Turbomach. | ASME Digital Collection

Topics: Blades , Boundary layers , Calibration , Cascades (Fluid dynamics) , Computer-aided engineering , Design , Diffusion (Physics) , Flow (Dynamics) , Mach number , Nozzles

A Model for Closing the Inviscid Form of the Average-Passage Equation System

J. J. Adamczyk, R. A. Mulac, M. L. Celestina

J. Turbomach. October 1986, 108(2): 180–186. doi: https://doi.org/10.1115/1.3262035

Abstract

View articletitled, A Model for Closing the Inviscid Form of the Average-Passage Equation System

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Topics: Blades , Computers , Design , Engineering simulation , Flow (Dynamics) , Propellers , Simulation , Turbomachinery

A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller

M. L. Celestina, R. A. Mulac, J. J. Adamczyk

J. Turbomach. October 1986, 108(2): 187–193. doi: https://doi.org/10.1115/1.3262036

Abstract

View articletitled, A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller

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Topics: Computer simulation , Inviscid flow , Propellers , Blades , Flow (Dynamics) , Simulation

An Inverse (Design) Problem Solution Method for the Blade Cascade Flow on Streamsurface of Revolution

Naixing Chen, Fengxian Zhang, Weihong Li

J. Turbomach. October 1986, 108(2): 194–199. doi: https://doi.org/10.1115/1.3262037

Abstract

View articletitled, An Inverse (Design) Problem Solution Method for the Blade Cascade Flow on Streamsurface of Revolution

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Topics: Blades , Design , Flow (Dynamics) , Tensors , Pressure , Suction , Cascades (Fluid dynamics) , Aerodynamics , Computational methods , Differential equations

A Method for Transonic Inverse Cascade Design With a Stream Function Equation

Manchu Ge, Yiping Lou, Zhengti Yu

J. Turbomach. October 1986, 108(2): 200–205. doi: https://doi.org/10.1115/1.3262038

Abstract

View articletitled, A Method for Transonic Inverse Cascade Design With a Stream Function Equation

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Topics: Cascades (Fluid dynamics) , Design , Blades , Suction , Transonic flow , Density , Design methodology , Entropy , Flow (Dynamics) , Pressure

Navier–Stokes Solutions of Unsteady Flow in a Compressor Rotor

J. N. Scott, W. L. Hankey, Jr.

J. Turbomach. October 1986, 108(2): 206–215. doi: https://doi.org/10.1115/1.3262039

Abstract

View articletitled, Navier–Stokes Solutions of Unsteady Flow in a Compressor Rotor

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Topics: Compressors , Rotors , Unsteady flow , Blades , Flow (Dynamics) , Turbulence , Outflow , Algebra , Algorithms , Computation

Axisymmetrically Stalled Flow Performance for Multistage Axial Compressors

S. G. Koff, E. M. Greitzer

J. Turbomach. October 1986, 108(2): 216–223. doi: https://doi.org/10.1115/1.3262040

Abstract

View articletitled, Axisymmetrically Stalled Flow Performance for Multistage Axial Compressors

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Topics: Compressors , Flow (Dynamics) , Pressure , Blades

Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

D. L. Tweedt, T. H. Okiishi, M. D. Hathaway

J. Turbomach. October 1986, 108(2): 224–232. doi: https://doi.org/10.1115/1.3262041

Abstract

View articletitled, Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

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Topics: Compressors , Stators , Clearances (Engineering) , Blades , Aerodynamics , Axial flow

Development of a High-Pressure-Ratio Axial Flow Compressor for a Medium-Size Gas Turbine

Y. Kashiwabara, Y. Matsuura, Y. Katoh, N. Hagiwara, T. Hattori, K. Tokunaga

J. Turbomach. October 1986, 108(2): 233–239. doi: https://doi.org/10.1115/1.3262042

Abstract

View articletitled, Development of a High-Pressure-Ratio Axial Flow Compressor for a Medium-Size Gas Turbine

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Topics: Axial flow , Gas turbines , Pressure , Compressors , Construction , Data acquisition systems , Design , Design engineering , Instrumentation

The “Axi-Fuge”—A Novel Compressor

J. O. Wiggins

J. Turbomach. October 1986, 108(2): 240–243. doi: https://doi.org/10.1115/1.3262043

Abstract

View articletitled, The “Axi-Fuge”—A Novel Compressor

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Topics: Compressors , Gas turbines , Thermal efficiency , Cycles , Heat exchangers , Air compressors , Design , Fuel consumption , Geometry , Solar energy

Splitter Blades as an Aeroelastic Detuning Mechanism for Unstalled Supersonic Flutter of Turbomachine Rotors

D. A. Topp, S. Fleeter

J. Turbomach. October 1986, 108(2): 244–252. doi: https://doi.org/10.1115/1.3262044

Abstract

View articletitled, Splitter Blades as an Aeroelastic Detuning Mechanism for Unstalled Supersonic Flutter of Turbomachine Rotors

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Topics: Blades , Flutter (Aerodynamics) , Rotors , Turbomachinery , Chords (Trusses) , Airfoils , Stability , Cascades (Fluid dynamics) , Design , Torsion

The Effect of Circumferential Aerodynamic Detuning on Coupled Bending-Torsion Unstalled Supersonic Flutter

D. Hoyniak, S. Fleeter

J. Turbomach. October 1986, 108(2): 253–260. doi: https://doi.org/10.1115/1.3262045

Abstract

View articletitled, The Effect of Circumferential Aerodynamic Detuning on Coupled Bending-Torsion Unstalled Supersonic Flutter

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Topics: Flutter (Aerodynamics) , Torsion , Stability , Center of mass , Rotors , Cascades (Fluid dynamics) , Degrees of freedom , Airfoils , Chords (Trusses) , Equations of motion

The Aerodynamic Development of a Highly Loaded Nozzle Guide Vane

N. C. Baines, M. L. G. Oldfield, J. P. Simons, J. M. Wright

J. Turbomach. October 1986, 108(2): 261–268. doi: https://doi.org/10.1115/1.3262046

Abstract

View articletitled, The Aerodynamic Development of a Highly Loaded Nozzle Guide Vane

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Topics: Nozzle guide vanes , Boundary layers , Blades , Cascades (Fluid dynamics) , Suction , Boundary layer turbulence , Design , Flowmeters , Frequency response , High pressure (Physics)

The Effect of a Downstream Rotor on the Measured Performance of a Transonic Turbine Nozzle

R. G. Williamson, S. H. Moustapha, J. P. Huot

J. Turbomach. October 1986, 108(2): 269–274. doi: https://doi.org/10.1115/1.3262047

Abstract

View articletitled, The Effect of a Downstream Rotor on the Measured Performance of a Transonic Turbine Nozzle

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Topics: Nozzles , Rotors , Turbines , Turning angles , Design , Exterior walls , Flow (Dynamics) , Mach number , Performance evaluation , Testing

Inverse Design of Composite Turbine Blade Circular Coolant Flow Passages

T.-L. Chiang, G. S. Dulikravich

J. Turbomach. October 1986, 108(2): 275–282. doi: https://doi.org/10.1115/1.3262048

Abstract

View articletitled, Inverse Design of Composite Turbine Blade Circular Coolant Flow Passages

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Topics: Composite materials , Coolants , Design , Flow (Dynamics) , Turbine blades , Blades , Optimization , Boundary element methods , Heat flux , Heat conduction

Small Diameter Film Cooling Holes: Wall Convective Heat Transfer

G. E. Andrews, M. Alikhanizadeh, A. A. Asere, C. I. Hussain, M. S. Khoshkbar Azari, M. C. Mkpadi

J. Turbomach. October 1986, 108(2): 283–289. doi: https://doi.org/10.1115/1.3262049

Abstract

View articletitled, Small Diameter Film Cooling Holes: Wall Convective Heat Transfer

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Topics: Combustion chambers , Convection , Coolants , Film cooling , Flow (Dynamics) , Gas turbines , Heat transfer , Metals , Turbine blades

Multistage Turbine Erosion

M. Menguturk, D. Gunes, M. Erten, E. F. Sverdrup

J. Turbomach. October 1986, 108(2): 290–297. doi: https://doi.org/10.1115/1.3262050

Abstract

View articletitled, Multistage Turbine Erosion

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Topics: Erosion , Turbines , Particulate matter , Blades , Computers , Rotors , Damage , Gas flow , Gas turbines , Gases

The Dynamics of Suspended Solid Particles in a Two-Stage Gas Turbine

W. Tabakoff, A. Hamed

J. Turbomach. October 1986, 108(2): 298–302. doi: https://doi.org/10.1115/1.3262051

Abstract

View articletitled, The Dynamics of Suspended Solid Particles in a Two-Stage Gas Turbine

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Topics: Dynamics (Mechanics) , Gas turbines , Particulate matter , Erosion , Turbine blades , Blades , Flow (Dynamics) , Turbines , Coal , Collisions (Physics)

A New Experimental Technique to Simulate Secondary Erosion in Turbine Cascades

P. J. Singh, J. L. Dussourd

J. Turbomach. October 1986, 108(2): 303–310. doi: https://doi.org/10.1115/1.3262052

Abstract

View articletitled, A New Experimental Technique to Simulate Secondary Erosion in Turbine Cascades

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Topics: Erosion , Turbines , Blades , Flow (Dynamics) , Particulate matter , Suction , Vortices , Damage , Dust , Boundary layers

Discussions

Discussion: “Extensive Verification of the Denton New Scheme From the User’s Point of View: Parts I and II” (Sato, T., Aoki, S., and Nagayama, T., 1986, ASME J. Turbomach., 108, pp. 162–177)

J. D. Denton

J. Turbomach. October 1986, 108(2): 177–178. doi: https://doi.org/10.1115/1.3262033

View articletitled, Discussion: “Extensive Verification of the Denton New Scheme From the User’s Point of View: Parts I and II” (Sato, T., Aoki, S., and Nagayama, T., 1986, ASME J. Turbomach., 108, pp. 162–177)

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Closure to “Discussion of ‘Extensive Verification of the Denton New Scheme From the User’s Point of View: Parts I and II’” (1986, ASME J. Turbomach., 108, pp. 177–178)

T. Sato, S. Aoki, T. Nagayama

J. Turbomach. October 1986, 108(2): 178–179. doi: https://doi.org/10.1115/1.3262034

View articletitled, Closure to “Discussion of ‘Extensive Verification of the Denton New Scheme From the User’s Point of View: Parts I and II’” (1986, ASME J. Turbomach., 108, pp. 177–178)

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Research Papers

Extensive Verification of the Denton New Scheme From the User’s Point of View: Part I—Calibration of Code Control Variables

Extensive Verification of the Denton New Scheme From the User’s Point of View: Part II—Comparison of Calculated and Experimental Results

A Model for Closing the Inviscid Form of the Average-Passage Equation System

A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller

An Inverse (Design) Problem Solution Method for the Blade Cascade Flow on Streamsurface of Revolution

A Method for Transonic Inverse Cascade Design With a Stream Function Equation

Navier–Stokes Solutions of Unsteady Flow in a Compressor Rotor

Axisymmetrically Stalled Flow Performance for Multistage Axial Compressors

Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance

Development of a High-Pressure-Ratio Axial Flow Compressor for a Medium-Size Gas Turbine

The “Axi-Fuge”—A Novel Compressor

Splitter Blades as an Aeroelastic Detuning Mechanism for Unstalled Supersonic Flutter of Turbomachine Rotors

The Effect of Circumferential Aerodynamic Detuning on Coupled Bending-Torsion Unstalled Supersonic Flutter

The Aerodynamic Development of a Highly Loaded Nozzle Guide Vane

The Effect of a Downstream Rotor on the Measured Performance of a Transonic Turbine Nozzle

Inverse Design of Composite Turbine Blade Circular Coolant Flow Passages

Small Diameter Film Cooling Holes: Wall Convective Heat Transfer

Multistage Turbine Erosion

The Dynamics of Suspended Solid Particles in a Two-Stage Gas Turbine

A New Experimental Technique to Simulate Secondary Erosion in Turbine Cascades

Discussions

Discussion: “Extensive Verification of the Denton New Scheme From the User’s Point of View: Parts I and II” (Sato, T., Aoki, S., and Nagayama, T., 1986, ASME J. Turbomach., 108, pp. 162–177)

Closure to “Discussion of ‘Extensive Verification of the Denton New Scheme From the User’s Point of View: Parts I and II’” (1986, ASME J. Turbomach., 108, pp. 177–178)

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