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Proceedings Papers

Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame

A. Amerini, S. Paccati, L. Mazzei, A. Andreini

Proc. ASME. GT2022, Volume 6A: Heat Transfer — Combustors; Film Cooling, V06AT11A001, June 13–17, 2022

Paper No: GT2022-81345

DOI: https://doi.org/10.1115/GT2022-81345

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Topics: Combustion chambers, Flames, Heat transfer, Physics, Simulation, Computational fluid dynamics, Cooling systems, Heat, Collaboration, Cooling

Proceedings Papers

Scale Resolving CFD Investigations of Aerothermal Field and Emissions of a Lean Burn Aeroengine Combustor

S. Paccati, L. Mazzei, A. Andreini, S. Patil, S. Shrivastava, D. Bessette, C. Arguinzoni, R. Yadav

Proc. ASME. GT2021, Volume 3A: Combustion, Fuels, and Emissions, V03AT04A054, June 7–11, 2021

Paper No: GT2021-59387

DOI: https://doi.org/10.1115/GT2021-59387

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Topics: Combustion chambers, Computational fluid dynamics, Emissions, Reynolds-averaged Navier–Stokes equations, Flames, Nitrogen oxides, Simulation, Aircraft engines, Boundary layers, Chemically reactive flow

Proceedings Papers

Reduced-Order Models for Effusion Modelling in Gas Turbine Combustors

S. Paccati, L. Mazzei, A. Andreini, B. Facchini

Proc. ASME. GT2021, Volume 5A: Heat Transfer — Combustors; Film Cooling, V05AT11A003, June 7–11, 2021

Paper No: GT2021-59384

DOI: https://doi.org/10.1115/GT2021-59384

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Topics: Combustion chambers, Gas turbines, Modeling, Computational fluid dynamics, Coolants, Cooling, Engineering simulation, Simulation, Temperature, Design

Journal Articles

Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow

T. Lenzi, L. Palanti, A. Picchi, T. Bacci, L. Mazzei, A. Andreini, B. Facchini

J. Turbomach. June 2020, 142(6): 061008.

Paper No: TURBO-19-1254

DOI: https://doi.org/10.1115/1.4046181

Published Online: May 28, 2020

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Topics: Computational fluid dynamics, Coolants, Flow (Dynamics), Jets, Swirling flow, Turbulence, Cooling, Pressure drop, Cooling systems, Vorticity

Proceedings Papers

Numerical Investigation on the Effect of Rotation and Holes Arrangement in Cold Bridge Type Impingement Cooling Systems

S. Paccati, L. Cocchi, L. Mazzei, A. Andreini

Proc. ASME. GT2019, Volume 5A: Heat Transfer, V05AT11A008, June 17–21, 2019

Paper No: GT2019-90770

DOI: https://doi.org/10.1115/GT2019-90770

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Topics: Bridges (Structures), Impingement cooling, Rotation, Heat transfer, Cavities, Coolants, Cooling, Flow (Dynamics), Blades, Cooling systems

Proceedings Papers

Multiphysics Numerical Investigation of an Aeronautical Lean Burn Combustor

D. Bertini, L. Mazzei, A. Andreini, B. Facchini

Proc. ASME. GT2019, Volume 5B: Heat Transfer, V05BT17A004, June 17–21, 2019

Paper No: GT2019-91437

DOI: https://doi.org/10.1115/GT2019-91437

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Topics: Combustion chambers, Design, Engineering simulation, Simulation, Cooling, Flow (Dynamics), Reynolds-averaged Navier–Stokes equations, Turbines, Combustion, Compressors

Proceedings Papers

Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow

T. Lenzi, L. Palanti, A. Picchi, T. Bacci, L. Mazzei, A. Andreini, B. Facchini, I. Vitale

Proc. ASME. GT2019, Volume 5B: Heat Transfer, V05BT19A016, June 17–21, 2019

Paper No: GT2019-91446

DOI: https://doi.org/10.1115/GT2019-91446

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Topics: Cooling systems, Flow (Dynamics), Swirling flow, Jets, Combustion chambers, Coolants, Cooling, Film cooling, Computational fluid dynamics, Eddies (Fluid dynamics)

Journal Articles

Impact of Predicted Combustor Outlet Conditions on the Aerothermal Performance of Film-Cooled High Pressure Turbine Vanes

S. Cubeda, L. Mazzei, T. Bacci, A. Andreini

J. Eng. Gas Turbines Power. May 2019, 141(5): 051011.

Paper No: GTP-18-1373

DOI: https://doi.org/10.1115/1.4041038

Published Online: December 12, 2018

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Topics: Airfoils, Combustion chambers, Flow (Dynamics), Reynolds-averaged Navier–Stokes equations, Simulation, Temperature, Turbines, Turbulence, Film cooling, Coolants

Journal Articles

Numerical and Experimental Investigation on an Effusion-Cooled Lean Burn Aeronautical Combustor: Aerothermal Field and Emissions

L. Mazzei, S. Puggelli, D. Bertini, A. Andreini, B. Facchini, I. Vitale, A. Santoriello

J. Eng. Gas Turbines Power. April 2019, 141(4): 041006.

Paper No: GTP-18-1587

DOI: https://doi.org/10.1115/1.4041676

Published Online: November 2, 2018

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Topics: Combustion chambers, Emissions, Temperature, Sprays, Flames, Combustion, Turbulence, Modeling, Fuels

Proceedings Papers

Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow

T. Bacci, T. Lenzi, A. Picchi, L. Mazzei, B. Facchini

Proc. ASME. GT2018, Volume 5C: Heat Transfer, V05CT17A009, June 11–15, 2018

Paper No: GT2018-76728

DOI: https://doi.org/10.1115/GT2018-76728

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Topics: Combustion chambers, Flow (Dynamics), High pressure (Physics), Outflow, Temperature, Turbines, Turbulence, Aircraft engines, Cooling, Nozzle guide vanes

Proceedings Papers

Numerical and Experimental Investigation on an Effusion-Cooled Lean Burn Aeronautical Combustor: Aerothermal Field and Metal Temperature

D. Bertini, L. Mazzei, S. Puggelli, A. Andreini, B. Facchini, L. Bellocci, A. Santoriello

Proc. ASME. GT2018, Volume 5C: Heat Transfer, V05CT17A010, June 11–15, 2018

Paper No: GT2018-76779

DOI: https://doi.org/10.1115/GT2018-76779

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Topics: Combustion chambers, Metals, Temperature, Combustion, Heat, Coolants, Cooling, Engineering simulation, Simulation, Stress

Proceedings Papers

Impact of Predicted Combustor Outlet Conditions on the Aerothermal Performance of Film-Cooled HPT Vanes

S. Cubeda, L. Mazzei, T. Bacci, A. Andreini

Proc. ASME. GT2018, Volume 5C: Heat Transfer, V05CT17A005, June 11–15, 2018

Paper No: GT2018-75921

DOI: https://doi.org/10.1115/GT2018-75921

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Topics: Combustion chambers, Reynolds-averaged Navier–Stokes equations, Turbines, Simulation, Design, Flow (Dynamics), Cooling systems, Stress, Temperature, Aerodynamics

Proceedings Papers

Numerical and Experimental Investigation on an Effusion-Cooled Lean Burn Aeronautical Combustor: Aerothermal Field and Emissions

L. Mazzei, S. Puggelli, D. Bertini, A. Andreini, B. Facchini, I. Vitale, A. Santoriello

Proc. ASME. GT2018, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A033, June 11–15, 2018

Paper No: GT2018-76765

DOI: https://doi.org/10.1115/GT2018-76765

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Topics: Combustion chambers, Emissions, Combustion, Nitrogen oxides, Pollution, Temperature profiles, Computational fluid dynamics, Cooling systems, Cycles, Design

Journal Articles

Modeling Strategies for Large Eddy Simulation of Lean Burn Spray Flames

S. Puggelli, D. Bertini, L. Mazzei, A. Andreini

J. Eng. Gas Turbines Power. May 2018, 140(5): 051501.

Paper No: GTP-17-1396

DOI: https://doi.org/10.1115/1.4038127

Published Online: November 21, 2017

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Topics: Combustion, Flamelet generated manifold, Flames, Modeling, Sprays, Fuels, Flow (Dynamics), Temperature, Turbulence, Pressure

Proceedings Papers

Numerical Investigation of Optimized Arrangements for Effusion Cooling in Gas Turbine Combustor Applications

L. Mazzei, S. Puggelli, A. Andreini, B. Facchini

Proc. ASME. GT2017, Volume 5C: Heat Transfer, V05CT17A012, June 26–30, 2017

Paper No: GT2017-65038

DOI: https://doi.org/10.1115/GT2017-65038

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Topics: Combustion chambers, Cooling, Gas turbines, Computational fluid dynamics, Coolants, Simulation, Acoustics, Aircraft engines, Boundary-value problems, Cooling systems

Proceedings Papers

Modelling Strategies for Large-Eddy Simulation of Lean Burn Spray Flames

S. Puggelli, D. Bertini, L. Mazzei, A. Andreini

Proc. ASME. GT2017, Volume 4B: Combustion, Fuels and Emissions, V04BT04A029, June 26–30, 2017

Paper No: GT2017-64569

DOI: https://doi.org/10.1115/GT2017-64569

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Topics: Flames, Large eddy simulation, Modeling, Sprays, Flamelet generated manifold, Combustion, Computational fluid dynamics, Pressure, Safety, Aircraft engines

Journal Articles

Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Numerical Investigation

E. Burberi, D. Massini, L. Cocchi, L. Mazzei, A. Andreini, B. Facchini

J. Turbomach. March 2017, 139(3): 031005.

Paper No: TURBO-16-1207

DOI: https://doi.org/10.1115/1.4034799

Published Online: November 16, 2016

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Topics: Blades, Cooling systems, Eddies (Fluid dynamics), Flow (Dynamics), Gas turbines, Heat transfer, Reynolds-averaged Navier–Stokes equations, Rotation, Simulation, Turbulence

Journal Articles

Hybrid RANS-LES Modeling of the Aerothermal Field in an Annular Hot Streak Generator for the Study of Combustor–Turbine Interaction

A. Andreini, T. Bacci, M. Insinna, L. Mazzei, S. Salvadori

J. Eng. Gas Turbines Power. February 2017, 139(2): 021508.

Paper No: GTP-16-1293

DOI: https://doi.org/10.1115/1.4034358

Published Online: September 20, 2016

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Topics: Combustion chambers, Flow (Dynamics), Reynolds-averaged Navier–Stokes equations, Temperature, Computational fluid dynamics, Turbines, Design, Modeling, Turbulence, Simulation

Proceedings Papers

Assessment of Scale Resolved CFD Methods for the Investigation of Lean Burn Spray Flames

A. Andreini, D. Bertini, L. Mazzei, S. Puggelli

Proc. ASME. GT2016, Volume 4A: Combustion, Fuels and Emissions, V04AT04A057, June 13–17, 2016

Paper No: GT2016-57143

DOI: https://doi.org/10.1115/GT2016-57143

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Topics: Computational fluid dynamics, Flames, Sprays, Simulation, Engineering simulation, Combustion, Flamelet generated manifold, Combustion chambers, Eddies (Fluid dynamics), Electrical discharge machining

Proceedings Papers

Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Numerical Investigation

E. Burberi, D. Massini, L. Cocchi, L. Mazzei, A. Andreini, B. Facchini

Proc. ASME. GT2016, Volume 5B: Heat Transfer, V05BT11A011, June 13–17, 2016

Paper No: GT2016-57178

DOI: https://doi.org/10.1115/GT2016-57178

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Topics: Blades, Cooling systems, Gas turbines, Rotation, Flow (Dynamics), Simulation, Heat transfer coefficients, Bridges (Structures), Coolants, Cooling

Journal citation

NARROW

Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame

Scale Resolving CFD Investigations of Aerothermal Field and Emissions of a Lean Burn Aeroengine Combustor

Reduced-Order Models for Effusion Modelling in Gas Turbine Combustors

Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow

Numerical Investigation on the Effect of Rotation and Holes Arrangement in Cold Bridge Type Impingement Cooling Systems

Multiphysics Numerical Investigation of an Aeronautical Lean Burn Combustor

Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow

Impact of Predicted Combustor Outlet Conditions on the Aerothermal Performance of Film-Cooled High Pressure Turbine Vanes

Numerical and Experimental Investigation on an Effusion-Cooled Lean Burn Aeronautical Combustor: Aerothermal Field and Emissions

Flow Field and Hot Streak Migration Through High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow

Numerical and Experimental Investigation on an Effusion-Cooled Lean Burn Aeronautical Combustor: Aerothermal Field and Metal Temperature

Impact of Predicted Combustor Outlet Conditions on the Aerothermal Performance of Film-Cooled HPT Vanes

Numerical and Experimental Investigation on an Effusion-Cooled Lean Burn Aeronautical Combustor: Aerothermal Field and Emissions

Modeling Strategies for Large Eddy Simulation of Lean Burn Spray Flames

Numerical Investigation of Optimized Arrangements for Effusion Cooling in Gas Turbine Combustor Applications

Modelling Strategies for Large-Eddy Simulation of Lean Burn Spray Flames

Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Numerical Investigation

Hybrid RANS-LES Modeling of the Aerothermal Field in an Annular Hot Streak Generator for the Study of Combustor–Turbine Interaction

Assessment of Scale Resolved CFD Methods for the Investigation of Lean Burn Spray Flames

Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Numerical Investigation

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