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Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSNConference contribution/Paperpeer-review

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Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections. / Castorrini, Alessio; Venturini, Paolo; Corsini, Alessandro.
Volume 1. Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers (ASME), 2021. GT2020-15379 (Proceedings of the ASME Turbo Expo; Vol. 1).

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSNConference contribution/Paperpeer-review

Harvard

Castorrini, A, Venturini, P & Corsini, A 2021, Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections. in Volume 1. Aircraft Engine; Fans and Blowers., GT2020-15379, Proceedings of the ASME Turbo Expo, vol. 1, American Society of Mechanical Engineers (ASME), ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020, Virtual, Online, 21/09/20. https://doi.org/10.1115/GT2020-15379

APA

Castorrini, A., Venturini, P., & Corsini, A. (2021). Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections. In Volume 1. Aircraft Engine; Fans and Blowers Article GT2020-15379 (Proceedings of the ASME Turbo Expo; Vol. 1). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT2020-15379

Vancouver

Castorrini A, Venturini P, Corsini A. Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections. In Volume 1. Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers (ASME). 2021. GT2020-15379. (Proceedings of the ASME Turbo Expo). doi: 10.1115/GT2020-15379

Author

Castorrini, Alessio ; Venturini, Paolo ; Corsini, Alessandro. / Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections. Volume 1. Aircraft Engine; Fans and Blowers. American Society of Mechanical Engineers (ASME), 2021. (Proceedings of the ASME Turbo Expo).

Bibtex

@inproceedings{f09e4278fb6944e7ae8635e54d0cf2b1,
title = "Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections",
abstract = "In the last decade, the authors focused their research in the development and implementation of accurate numerical tools and methods able to predict the erosion and deposit on turbomachinery blades operating with particle-laden flows. These models and methods give complete three-dimensional description of the phenomenon, but their application is limited to a single working condition of the blade. The present paper covers the first step in the definition of a general methodology to extend the applicability of these tools to a full range of the machines operating conditions. The method aims to obtain an instantaneous prediction of the expected damage pattern for a blade section, given its local working condition in terms of relative fluid-particle flow. The final result is based on a precomputed database associated to the blade section, where the single element is obtained by computing the erosion damage using the aforementioned numerical tools. This paper will show the methodology to obtain the database associated to the midspan section of an induced draft fan subjected to erosion due to coal ash particle. The final database is then used to predict the damage state of the section associated to a given point in the characteristic curve of the fan.",
keywords = "Erosion/deposition prediction, Fan, Particle-laden flow",
author = "Alessio Castorrini and Paolo Venturini and Alessandro Corsini",
year = "2021",
month = jan,
day = "11",
doi = "10.1115/GT2020-15379",
language = "English",
series = "Proceedings of the ASME Turbo Expo",
publisher = "American Society of Mechanical Engineers (ASME)",
booktitle = "Volume 1. Aircraft Engine; Fans and Blowers",
note = "ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020 ; Conference date: 21-09-2020 Through 25-09-2020",

}

RIS

TY - GEN

T1 - Integration of computational fluid-particle dynamics techniques for the instantaneous estimation of particle erosion damage on axial fan blade sections

AU - Castorrini, Alessio

AU - Venturini, Paolo

AU - Corsini, Alessandro

PY - 2021/1/11

Y1 - 2021/1/11

N2 - In the last decade, the authors focused their research in the development and implementation of accurate numerical tools and methods able to predict the erosion and deposit on turbomachinery blades operating with particle-laden flows. These models and methods give complete three-dimensional description of the phenomenon, but their application is limited to a single working condition of the blade. The present paper covers the first step in the definition of a general methodology to extend the applicability of these tools to a full range of the machines operating conditions. The method aims to obtain an instantaneous prediction of the expected damage pattern for a blade section, given its local working condition in terms of relative fluid-particle flow. The final result is based on a precomputed database associated to the blade section, where the single element is obtained by computing the erosion damage using the aforementioned numerical tools. This paper will show the methodology to obtain the database associated to the midspan section of an induced draft fan subjected to erosion due to coal ash particle. The final database is then used to predict the damage state of the section associated to a given point in the characteristic curve of the fan.

AB - In the last decade, the authors focused their research in the development and implementation of accurate numerical tools and methods able to predict the erosion and deposit on turbomachinery blades operating with particle-laden flows. These models and methods give complete three-dimensional description of the phenomenon, but their application is limited to a single working condition of the blade. The present paper covers the first step in the definition of a general methodology to extend the applicability of these tools to a full range of the machines operating conditions. The method aims to obtain an instantaneous prediction of the expected damage pattern for a blade section, given its local working condition in terms of relative fluid-particle flow. The final result is based on a precomputed database associated to the blade section, where the single element is obtained by computing the erosion damage using the aforementioned numerical tools. This paper will show the methodology to obtain the database associated to the midspan section of an induced draft fan subjected to erosion due to coal ash particle. The final database is then used to predict the damage state of the section associated to a given point in the characteristic curve of the fan.

KW - Erosion/deposition prediction

KW - Fan

KW - Particle-laden flow

U2 - 10.1115/GT2020-15379

DO - 10.1115/GT2020-15379

M3 - Conference contribution/Paper

AN - SCOPUS:85099791663

T3 - Proceedings of the ASME Turbo Expo

BT - Volume 1. Aircraft Engine; Fans and Blowers

PB - American Society of Mechanical Engineers (ASME)

T2 - ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020

Y2 - 21 September 2020 through 25 September 2020

ER -