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Journal Articles

Influence of Gap Shape on Flow Characteristics of Highly Loaded Compressor Tandem Cascades

Xiaochen Mao, Yingchen Jiao, Hao Cheng, Botao Zhang, Bo Liu

Publisher: ASME

J. Eng. Gas Turbines Power. September 2024, 146(9): 091016.

Paper No: GTP-23-1583

https://doi.org/10.1115/1.4065019

Published Online: April 4, 2024

View Articletitled, Influence of Gap Shape on Flow Characteristics of Highly Loaded Compressor Tandem Cascades

Topics: Blades, Cascades (Fluid dynamics), Corners (Structural elements), Flow (Dynamics), Design, Shapes, Numerical analysis, Compressors, Stress

Journal Articles

Periodic Unsteady Kinematics of Hub Flows in a Shrouded Multistage Compressor

Jaehyoung Lee, Sungkyung Lim, Hyoun-Woo Shin, Sungryong Lee, Seung Jin Song

Publisher: ASME

J. Eng. Gas Turbines Power. April 2022, 144(4): 041011.

Paper No: GTP-21-1571

https://doi.org/10.1115/1.4053106

Published Online: January 21, 2022

View Articletitled, Periodic Unsteady Kinematics of Hub Flows in a Shrouded Multistage Compressor

Topics: Compressors, Flow (Dynamics), Rotors, Stators, Wakes, Corners (Structural elements), Separation (Technology), Vorticity

Journal Articles

The Effect of the Degree of Premixedness on Self-Excited Combustion Instability

Adam Howie, Daniel Doleiden, Stephen Peluso, Jacqueline O'Connor

Publisher: ASME

J. Eng. Gas Turbines Power. July 2021, 143(7): 071024.

Paper No: GTP-20-1458

https://doi.org/10.1115/1.4049486

Published Online: March 31, 2021

View Articletitled, The Effect of the Degree of Premixedness on Self-Excited Combustion Instability

Topics: Combustion chambers, Flames, Fluctuations (Physics), Nozzles, Oscillations, Heat, Fuels, Pressure, Dynamics (Mechanics), Combustion

Journal Articles

Design Optimization of a Blended Blade and Endwall in a Compressor Cascade

Jiabin Li, Lucheng Ji, Ling Zhou

Publisher: ASME

J. Eng. Gas Turbines Power. February 2020, 142(2): 021003.

Paper No: GTP-19-1620

https://doi.org/10.1115/1.4045586

Published Online: January 6, 2020

View Articletitled, Design Optimization of a Blended Blade and Endwall in a Compressor Cascade

Topics: Blades, Cascades (Fluid dynamics), Design, Flow (Dynamics), Optimization, Pressure, Support vector machines, Corners (Structural elements), Compressors

Journal Articles

On the Influence of the Entrance Section on the Rotordynamic Performance of a Pump Seal With Uniform Clearance: A Sharp Edge Versus A Round Inlet

Jing Yang, Luis San Andrés

Publisher: ASME

J. Eng. Gas Turbines Power. March 2019, 141(3): 031029.

Paper No: GTP-18-1343

https://doi.org/10.1115/1.4040742

Published Online: December 4, 2018

View Articletitled, On the Influence of the Entrance Section on the Rotordynamic Performance of a Pump Seal With Uniform Clearance: A Sharp Edge Versus A Round Inlet

Topics: Clearances (Engineering), Computational fluid dynamics, Corners (Structural elements), Flow (Dynamics), Leakage, Pressure, Rotors, Pressure drop, Stiffness

Journal Articles

Predicting Gas Leakage in the Rotary Engine—Part I: Apex and Corner Seals

Mathieu Picard, Tian Tian, Takayuki Nishino

Publisher: ASME

J. Eng. Gas Turbines Power. June 2016, 138(6): 062503.

Paper No: GTP-15-1444

https://doi.org/10.1115/1.4031873

Published Online: November 17, 2015

View Articletitled, Predicting Gas Leakage in the Rotary Engine—Part I: Apex and Corner Seals

Topics: Clearances (Engineering), Corners (Structural elements), Gas flow, Leakage, Pressure, Engines, Rotors, Dynamics (Mechanics), Flow (Dynamics)

Journal Articles

Predicting Gas Leakage in the Rotary Engine—Part II: Side Seals and Summary

Mathieu Picard, Tian Tian, Takayuki Nishino

Publisher: ASME

J. Eng. Gas Turbines Power. June 2016, 138(6): 062504.

Paper No: GTP-15-1445

https://doi.org/10.1115/1.4031874

Published Online: November 17, 2015

View Articletitled, Predicting Gas Leakage in the Rotary Engine—Part II: Side Seals and Summary

Topics: Leakage, Corners (Structural elements), Pressure, Engines, Rotors

Journal Articles

Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor With Representative Swirling Flow

Antonio Andreini, Bruno Facchini, Riccardo Becchi, Alessio Picchi, Fabio Turrini

Publisher: ASME

J. Eng. Gas Turbines Power. April 2016, 138(4): 041501.

Paper No: GTP-15-1288

https://doi.org/10.1115/1.4031434

Published Online: October 13, 2015

View Articletitled, Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor With Representative Swirling Flow

Topics: Combustion chambers, Coolants, Cooling, Flow (Dynamics), Heat transfer, Ejectors, Pressure drop, Swirling flow, Heat transfer coefficients, Corners (Structural elements)

Journal Articles

Characteristics of Discharge Coefficient in a Rotating Disk System

D. J. Maeng, J. S. Lee, R. Jakoby, S. Kim, S. Wittig

Publisher: ASME

J. Eng. Gas Turbines Power. October 1999, 121(4): 663–669.

https://doi.org/10.1115/1.2818523

Published Online: October 1, 1999

View Articletitled, Characteristics of Discharge Coefficient in a Rotating Disk System

Topics: Discharge coefficient, Rotating disks, Rotors, Cavities, Disks, Pressure, Compressibility, Corners (Structural elements), Flow (Dynamics), Laser Doppler anemometry

Journal Articles

Damage Tolerance Based Life Prediction in Gas Turbine Engine Blades Under Vibratory High Cycle Fatigue

D. P. Walls, R. E. deLaneuville, S. E. Cunningham

Publisher: ASME

J. Eng. Gas Turbines Power. January 1997, 119(1): 143–146.

https://doi.org/10.1115/1.2815538

Published Online: January 1, 1997

View Articletitled, Damage Tolerance Based Life Prediction in Gas Turbine Engine Blades Under Vibratory High Cycle Fatigue

Topics: Blades, Damage, Gas turbines, High cycle fatigue, Fracture (Materials), Stress, Fracture mechanics, Algorithms, Corners (Structural elements), Crack propagation

Journal Articles

Slot and Vertical Face Grinding of Aerospace Components

R. B. Mindek, Jr., T. D. Howes

Publisher: ASME

J. Eng. Gas Turbines Power. July 1996, 118(3): 620–625.

https://doi.org/10.1115/1.2816693

Published Online: July 1, 1996

View Articletitled, Slot and Vertical Face Grinding of Aerospace Components

Topics: Aerospace industry, Grinding, Wheels, Damage, Wear, Corners (Structural elements), Grinding wheels, Heat, Boron, Tool steel

Journal Articles

Surface Integral and Finite Element Hybrid Method for Three-Dimensional Analysis of Arbitrarily Shaped Surface Cracks

W. D. Keat, D. M. Maybury, B. S. Annigeri

Publisher: ASME

J. Eng. Gas Turbines Power. April 1996, 118(2): 406–410.

https://doi.org/10.1115/1.2816604

Published Online: April 1, 1996

View Articletitled, Surface Integral and Finite Element Hybrid Method for Three-Dimensional Analysis of Arbitrarily Shaped Surface Cracks

Topics: Finite element analysis, Surface cracks, Fracture (Materials), Boundary-value problems, Corners (Structural elements), Finite element model, Modeling, Stress, Structural elements (Construction), Traction

Journal Articles

Flow Separation in Shock Wave Boundary Layer Interactions

A. Hamed, A. Kumar

Publisher: ASME

J. Eng. Gas Turbines Power. January 1994, 116(1): 98–103.

https://doi.org/10.1115/1.2906816

Published Online: January 1, 1994

View Articletitled, Flow Separation in Shock Wave Boundary Layer Interactions

Topics: Boundary layers, Flow separation, Shock waves, Separation (Technology), Boundary layer turbulence, Compression, Cooling, Corners (Structural elements), Cylinders, Databases

Journal Articles

Axial Compressor Stator Aerodynamics

H. D. Joslyn, R. P. Dring

Publisher: ASME

J. Eng. Gas Turbines Power. April 1985, 107(2): 485–492.

https://doi.org/10.1115/1.3239754

Published Online: April 1, 1985

View Articletitled, Axial Compressor Stator Aerodynamics

Topics: Aerodynamics, Compressors, Stators, Flow (Dynamics), Design, Turbomachinery, Airfoils, Corners (Structural elements), Flow visualization, Pressure

Journal Articles

Inlet Boundary Layer Effects in an Axial Compressor Rotor: Part I—Blade-to-Blade Effects

J. H. Wagner, R. P. Dring, H. D. Joslyn

Publisher: ASME

J. Eng. Gas Turbines Power. April 1985, 107(2): 374–380.

https://doi.org/10.1115/1.3239734

Published Online: April 1, 1985

View Articletitled, Inlet Boundary Layer Effects in an Axial Compressor Rotor: Part I—Blade-to-Blade Effects

Topics: Blades, Boundary layers, Compressors, Rotors, Flow (Dynamics), Corners (Structural elements), Flow visualization

Journal Articles

Inlet Boundary Layer Effects in an Axial Compressor Rotor: Part II—Throughflow Effects

J. H. Wagner, R. P. Dring, H. D. Joslyn

Publisher: ASME

J. Eng. Gas Turbines Power. April 1985, 107(2): 381–386.

https://doi.org/10.1115/1.3239735

Published Online: April 1, 1985

View Articletitled, Inlet Boundary Layer Effects in an Axial Compressor Rotor: Part II—Throughflow Effects

Topics: Boundary layers, Compressors, Rotors, Pressure, Blades, Corners (Structural elements), Flow (Dynamics), Fluids, Leakage

Journal Articles

Pressure Loss Through Sharp 180 Deg Turns in Smooth Rectangular Channels

D. E. Metzger, C. W. Plevich, C. S. Fan

Publisher: ASME

J. Eng. Gas Turbines Power. July 1984, 106(3): 677–681.

https://doi.org/10.1115/1.3239623

Published Online: July 1, 1984

View Articletitled, Pressure Loss Through Sharp 180 Deg Turns in Smooth Rectangular Channels

Topics: Pressure, Geometry, Airfoils, Flow (Dynamics), Clearances (Engineering), Coolants, Cooling, Corners (Structural elements), Gas turbines, Reynolds number

Journal Articles

Modifications of the Ives-Liutermoza Conformal-Mapping Procedure for Turbomachinery Cascades

W. J. Rae

Publisher: ASME

J. Eng. Gas Turbines Power. April 1984, 106(2): 445–448.

https://doi.org/10.1115/1.3239586

Published Online: April 1, 1984

View Articletitled, Modifications of the Ives-Liutermoza Conformal-Mapping Procedure for Turbomachinery Cascades

Topics: Blades, Cascades (Fluid dynamics), Compressors, Corners (Structural elements), Flow (Dynamics), Turbines, Turbomachinery

Journal Articles

An Improved Time-Marching Method for Turbomachinery Flow Calculation

J. D. Denton

Publisher: ASME

J. Eng. Gas Turbines Power. July 1983, 105(3): 514–521.

https://doi.org/10.1115/1.3227444

Published Online: July 1, 1983

View Articletitled, An Improved Time-Marching Method for Turbomachinery Flow Calculation

Topics: Flow (Dynamics), Turbomachinery, Entropy, Blades, Corners (Structural elements), Errors, Shock (Mechanics)

Journal Articles

Secondary Flow Mixing Losses in a Centrifugal Impeller

M. W. Johnson, J. Moore

Publisher: ASME

J. Eng. Gas Turbines Power. January 1983, 105(1): 24–32.

https://doi.org/10.1115/1.3227394

Published Online: January 1, 1983

View Articletitled, Secondary Flow Mixing Losses in a Centrifugal Impeller

Topics: Flow (Dynamics), Impellers, Boundary layers, Flow measurement, Separation (Technology), Wakes, Blades, Corners (Structural elements), Probes, Suction

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Influence of Gap Shape on Flow Characteristics of Highly Loaded Compressor Tandem Cascades

Periodic Unsteady Kinematics of Hub Flows in a Shrouded Multistage Compressor

The Effect of the Degree of Premixedness on Self-Excited Combustion Instability

Design Optimization of a Blended Blade and Endwall in a Compressor Cascade

On the Influence of the Entrance Section on the Rotordynamic Performance of a Pump Seal With Uniform Clearance: A Sharp Edge Versus A Round Inlet

Predicting Gas Leakage in the Rotary Engine—Part I: Apex and Corner Seals

Predicting Gas Leakage in the Rotary Engine—Part II: Side Seals and Summary

Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean-Burn Combustor With Representative Swirling Flow

Characteristics of Discharge Coefficient in a Rotating Disk System

Damage Tolerance Based Life Prediction in Gas Turbine Engine Blades Under Vibratory High Cycle Fatigue

Slot and Vertical Face Grinding of Aerospace Components

Surface Integral and Finite Element Hybrid Method for Three-Dimensional Analysis of Arbitrarily Shaped Surface Cracks

Flow Separation in Shock Wave Boundary Layer Interactions

Axial Compressor Stator Aerodynamics

Inlet Boundary Layer Effects in an Axial Compressor Rotor: Part I—Blade-to-Blade Effects

Inlet Boundary Layer Effects in an Axial Compressor Rotor: Part II—Throughflow Effects

Pressure Loss Through Sharp 180 Deg Turns in Smooth Rectangular Channels

Modifications of the Ives-Liutermoza Conformal-Mapping Procedure for Turbomachinery Cascades

An Improved Time-Marching Method for Turbomachinery Flow Calculation

Secondary Flow Mixing Losses in a Centrifugal Impeller

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