Preprint Article Version 1 This version is not peer-reviewed

Sediment Abrasion Mechanism at the Leading Edge of an Airfoil: Insights from NACA0012 Wear Tests

Version 1 : Received: 24 October 2024 / Approved: 25 October 2024 / Online: 25 October 2024 (11:49:59 CEST)

How to cite: Liu, Z.; Zhu, L.; Li, Y. T.; Lu, L.; Wang, P. W.; Meng, L. Sediment Abrasion Mechanism at the Leading Edge of an Airfoil: Insights from NACA0012 Wear Tests. Preprints 2024, 2024102034. https://doi.org/10.20944/preprints202410.2034.v1 Liu, Z.; Zhu, L.; Li, Y. T.; Lu, L.; Wang, P. W.; Meng, L. Sediment Abrasion Mechanism at the Leading Edge of an Airfoil: Insights from NACA0012 Wear Tests. Preprints 2024, 2024102034. https://doi.org/10.20944/preprints202410.2034.v1

Abstract

Multiple engineering projects have confirmed that hydraulic machinery operating in sediment-laden rivers suffers from sediment abrasion. Guide vanes are among the most severely worn flow-passing components and have long been a key research focus in hydraulic machinery. This study conducted wear tests using asymmetric incoming flow with a 10° impact angle and an NACA0012 aluminum alloy airfoil as the research object. The development of wear was analyzed, revealing that it primarily occurs at the airfoil’s leading edge and progresses through three stages: initiation, development, and stabilization. The Finnie model was used to analyze the initial wear mechanism, with calculated results closely matching the latest wear outcomes. In the initial stage, wear rate density was influenced by particle impact velocity, angle, volume fraction, and y-direction shear stress. A low-velocity zone near the impact point, combined with rebounding particles causing secondary impacts, increases particle volume fraction and wear rate density. These secondary impacts are the primary causes of wear on both the upstream and downstream surfaces. Furthermore, flow separation downstream of the leading edge makes this region highly susceptible to wear. This study provides valuable insights for addressing wear in hydraulic machinery for practical engineering applications.

Keywords

airfoil; near-wall region; wear; numerical simulation; wear mechanism; flow characteristics

Subject

Engineering, Energy and Fuel Technology

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