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    Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 004:;page 041006-1
    Author(s): Bacci, Tommaso; Picchi, Alessio; Lenzi, Tommaso; Facchini, Bruno; Innocenti, Luca
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Surface roughness is well known to significantly influence turbine aerodynamics and heat transfer; different studies have been undertaken in the last decades, in order to precisely characterize its effects and pursue a ...
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    Development and Application of an Internal Heat Transfer Measurement Technique for Cooled Real Engine Components1 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 010:;page 0101018-1
    Author(s): Ali, Asif; Cocchi, Lorenzo; Picchi, Alessio; Facchini, Bruno; Cubeda, Simone
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aim of this work is to present the development and application of a measurement technique that allows to record internal heat transfer features of real components. In order to apply this method, based on similar ...
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    Analysis of Swirl Number Effects on Effusion Flow Behavior Using Time-Resolved Particle Image Velocimetry 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 008:;page 81001-1
    Author(s): Lenzi, Tommaso; Picchi, Alessio; Andreini, Antonio; Facchini, Bruno
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The analysis of the interaction between the swirling and cooling flows, promoted by the liner film cooling system, is a fundamental task for the design of turbine combustion chambers since it influences different aspects ...
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    Experimental Investigation of the Flow Field and the Heat Transfer on a Scaled Cooled Combustor Liner With Realistic Swirling Flow Generated by a Lean Burn Injection System 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 003:;page 31012
    Author(s): Andreini, Antonio; Caciolli, Gianluca; Facchini, Bruno; Picchi, Alessio; Turrini, Fabio
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Leanburn swirl stabilized combustors represent the key technology to reduce NOx emissions in modern aircraft engines. The high amount of air admitted through a leanburn injection system is characterized by very complex ...
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    Experimental and Theoretical Investigation of Thermal Effectiveness in Multiperforated Plates for Combustor Liner Effusion Cooling 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 009:;page 91003
    Author(s): Andreini, Antonio; Facchini, Bruno; Picchi, Alessio; Tarchi, Lorenzo; Turrini, Fabio
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stateoftheart liner cooling technology for modern combustors is represented by effusion cooling (or fullcoverage film cooling). Effusion is a very efficient cooling strategy based on the use of multiperforated liners, where ...
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    Effect of Slot Injection and Effusion Array on the Liner Heat Transfer Coefficient of a Scaled Lean Burn Combustor With Representative Swirling Flow 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 004:;page 41501
    Author(s): Andreini, Antonio; Facchini, Bruno; Becchi, Riccardo; Picchi, Alessio; Turrini, Fabio
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: International standards regarding polluting emissions from civil aircraft engines are becoming gradually even more stringent. Nowadays, the most prominent way to meet the target of reducing NOx emissions in modern aeroengine ...
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    Adiabatic Effectiveness on High-Pressure Turbine Nozzle Guide Vanes Under Realistic Swirling Conditions 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 001:;page 11009
    Author(s): Bacci, Tommaso; Becchi, Riccardo; Picchi, Alessio; Facchini, Bruno
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In modern lean-burn aero-engine combustors, highly swirling flow structures are adopted to control the fuel-air mixing and to provide the correct flame stabilization mechanisms. Aggressive swirl fields and high turbulence ...
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    Flow Field and Hot Streak Migration Through a High Pressure Cooled Vanes With Representative Lean Burn Combustor Outflow 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 004:;page 41020
    Author(s): Bacci, Tommaso; Lenzi, Tommaso; Picchi, Alessio; Mazzei, Lorenzo; Facchini, Bruno
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Modern lean burn aero-engine combustors make use of relevant swirl degrees for flame stabilization. Moreover, important temperature distortions are generated, in tangential and radial directions, due to discrete fuel ...
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    Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007:;page 71010-1
    Author(s): Bacci, Tommaso; Picchi, Alessio; Babazzi, Giulia; Facchini, Bruno; Cubeda, Simone
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Combustor exit conditions in modern gas turbines are generally characterized by significant temperature distortions and swirl degree, which in turn is responsible for very high turbulence intensities. These distortions ...
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    Experimental Analysis of Additively Manufactured Latticework Coupons 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 006:;page 61001-1
    Author(s): Castelli, Niccolò; Sandri, Umberto; Picchi, Alessio; Facchini, Bruno; Morante, Francesco; Cubeda, Simone
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The capabilities and the precision of additive manufacturing processes have been tremendously increased in the last years, and this trend is not expected to be close to an end. Researchers, in the gas turbine industry, are ...
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