Improvement of solid particle erosion resistance of helicopter rotor blade with hybrid composite shield

Özen, İsmail; Gedikli, Hasan; Öztürk, Bülent

doi:10.1016/j.engfailanal.2020.105175

Cited by 6 publications

(2 citation statements)

References 59 publications

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“…The erosion resistance of TPU@G/Cx was evaluated through solid particle erosion tests. 43 As is well known, the erosion resistance of materials is related to many factors, such as ller content, surface treatment, roughness, and mechanical properties, as well as the shape, size, and hardness of the erodent, and also the erosion conditions (impingement angle, particle feed rate, ambient temperature, erosion distance), and so on. [44][45][46] In this study, solid particle erosion performance was investigated (Fig.…”

Section: Solid Particle Erosion Performancementioning

confidence: 99%

Polyurethane-based nanocomposite film with thermal deicing capability and anti-erosion for wind turbine blades protection in extreme environments

Cui,

Zhang,

Huang

et al. 2023

J. Mater. Chem. A

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Section: Solid Particle Erosion Performancementioning

confidence: 99%

Polyurethane-based nanocomposite film with thermal deicing capability and anti-erosion for wind turbine blades protection in extreme environments

Cui,

Zhang,

Huang

et al. 2023

J. Mater. Chem. A

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“…Thus far, many authors have investigated the solid particle erosion experimentally and/or numerically in complex curved surface parts used in these industries such as helicopter rotor blades, gas turbine engine compressor/turbine blades, pipe elbows and valves, and leadingedge slats, etc. [8][9][10][11][12][13][14][15].…”

Section: Introductionmentioning

confidence: 99%

Investigation on Solid Particle Erosion Performance of Aluminum Alloy Materials for Leading-Edge Slat

Budur,

Özen,

Öztürk

et al. 2024

Tribol. Ind.

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This study aims to characterize solid particle erosion behaviors of three different aluminum alloys (AA2024-T351, AA6061-T651, and AA7075-T651) and reveal their erosion performances on leading-edge slat of airplane wings. Solid particle erosion tests were conducted using silicon carbide erodent particles under the conditions of six different impingement angles (20°-90°) and four different impact velocities (70-192 m/s). The erosion simulations of a leading-edge slat of the aforementioned aluminum alloys were numerically simulated at four different rotation angles (0°-15°) for three different impact velocities (130-250 m/s). A commercial ANSYS Fluent software using the Euler-Lagrange equation and an experimental data-based erosion model was used for the erosion simulations. The experimental results showed that the erosion rate increases with increasing impact velocity and the maximum erosion rate is obtained at the impingement angle of 30° which reflects the ductile manner. Of the three aluminum alloys, the AA6061-T651 exhibited the worst erosion behavior followed by the AA2024-T351 sample, whereas the AA7075-T651 had the best erosion resistance. The numerical results indicated that the erosion rate values of slat surfaces made up of three different aluminum alloys showed a slight increase after a slat rotation angle of 5°.

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An experimental and numerical study of the solid particle erosion damage in an industrial cement large-sized fan

Fortini

Suman

Zanini

2023

Engineering Failure Analysis

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Improvement of solid particle erosion resistance of helicopter rotor blade with hybrid composite shield

Cited by 6 publications

References 59 publications

Polyurethane-based nanocomposite film with thermal deicing capability and anti-erosion for wind turbine blades protection in extreme environments

Polyurethane-based nanocomposite film with thermal deicing capability and anti-erosion for wind turbine blades protection in extreme environments

Investigation on Solid Particle Erosion Performance of Aluminum Alloy Materials for Leading-Edge Slat

An experimental and numerical study of the solid particle erosion damage in an industrial cement large-sized fan

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