Modeling of Particle Trajectory and Erosion of Large Rotor Blades

When operating in hostile environments, engines components are facing a serious problem of erosion, leading to a drastic drop in aerodynamic performance and life-cycle. This paper outlines the modeling and simulation of particle trajectory and erosion induced by sand particles. The governing equatio...

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Main Author: Adel Ghenaiet
Format: Article
Language:English
Published: Wiley 2016-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2016/7928347
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author Adel Ghenaiet
author_facet Adel Ghenaiet
author_sort Adel Ghenaiet
collection DOAJ
description When operating in hostile environments, engines components are facing a serious problem of erosion, leading to a drastic drop in aerodynamic performance and life-cycle. This paper outlines the modeling and simulation of particle trajectory and erosion induced by sand particles. The governing equations of particle dynamics through the moving of large rotor blades are introduced and solved separately from the flow field by using our in-house particle tracking code based on the finite element method. As the locations of impacts are predicted, the erosion is assessed by semiempirical correlations in terms of impact conditions and particle and target surface characteristics. The results of these computations carried out for different concentrations of suspended dust (sand) cloud generated at takeoff conditions reveal the main areas of impacts with high rates of erosion seen over a large strip from the blade suction side, around the leading edge and the pressure side of blade. The assessment of the blade geometry deterioration reveals that the upper corner of blade suffers from an intense erosion wear.
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spelling doaj-art-a9f8e2a0100348ed884094a88c4409fb2025-08-20T03:39:36ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742016-01-01201610.1155/2016/79283477928347Modeling of Particle Trajectory and Erosion of Large Rotor BladesAdel Ghenaiet0Faculty of Mechanical and Process Engineering, University of Sciences and Technology (USTHB), BP 32, El-Alia, Bab-Ezzouar, 16111 Algiers, AlgeriaWhen operating in hostile environments, engines components are facing a serious problem of erosion, leading to a drastic drop in aerodynamic performance and life-cycle. This paper outlines the modeling and simulation of particle trajectory and erosion induced by sand particles. The governing equations of particle dynamics through the moving of large rotor blades are introduced and solved separately from the flow field by using our in-house particle tracking code based on the finite element method. As the locations of impacts are predicted, the erosion is assessed by semiempirical correlations in terms of impact conditions and particle and target surface characteristics. The results of these computations carried out for different concentrations of suspended dust (sand) cloud generated at takeoff conditions reveal the main areas of impacts with high rates of erosion seen over a large strip from the blade suction side, around the leading edge and the pressure side of blade. The assessment of the blade geometry deterioration reveals that the upper corner of blade suffers from an intense erosion wear.http://dx.doi.org/10.1155/2016/7928347
spellingShingle Adel Ghenaiet
Modeling of Particle Trajectory and Erosion of Large Rotor Blades
International Journal of Aerospace Engineering
title Modeling of Particle Trajectory and Erosion of Large Rotor Blades
title_full Modeling of Particle Trajectory and Erosion of Large Rotor Blades
title_fullStr Modeling of Particle Trajectory and Erosion of Large Rotor Blades
title_full_unstemmed Modeling of Particle Trajectory and Erosion of Large Rotor Blades
title_short Modeling of Particle Trajectory and Erosion of Large Rotor Blades
title_sort modeling of particle trajectory and erosion of large rotor blades
url http://dx.doi.org/10.1155/2016/7928347
work_keys_str_mv AT adelghenaiet modelingofparticletrajectoryanderosionoflargerotorblades