Two-step simulation approach for laser shock peening

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Two-step simulation approach for laser shock peening. / Pozdnyakov, Vasily; Keller, Sören; Kashaev, Nikolai et al.
In: Proceedings in applied mathematics and mechanics, Vol. 19, No. 1, e201900497, 11.2019.

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@article{2242c88e3313457d8baa7dd22d503493,
title = "Two-step simulation approach for laser shock peening",
abstract = "Laser shock peening (LSP) is a surface modification technique to introduce compressive residual stresses (RS) with a high magnitude in the near surface region of the material. Due to non-linear interactions (e.g. laser absorption by plasma, shock wave propagation, etc.) and a high number of parameters, it is difficult to study and optimize the process based on experiments alone. Therefore, a two-step simulation approach is proposed in this paper, where two models are combined, because one model of the complete process is difficult to derive, due to the different characteristics of the plasma formation and the shockwave propagation in the material. On one hand, a global model including plasma and shock wave descriptions is applied for the LSP of an aluminium sample with water confinement. The numerical solution of this model, applied for a 3×3 mm2focus size, 5 J and 20 ns (full width at half maximum (FWHM)) laser pulse, allows to determine the temporal plasma pressure evolution on the material surface. On the other hand, a finite element simulation is used to calculate the RS distribution within the target material, where the plasma pressure is applied as a surface loading for the aluminium alloy AA2198-T3. The simulated residual stresses are fitted to measurements via parameter variation of the global model. The identified values and the two-step simulation approach can be used in future work to predict stress states of materials after LSP for various processparameters variations.",
keywords = "Engineering",
author = "Vasily Pozdnyakov and S{\"o}ren Keller and Nikolai Kashaev and Benjamin Klusemann and Jens Oberrath",
year = "2019",
month = nov,
doi = "10.1002/pamm.201900497",
language = "English",
volume = "19",
journal = "Proceedings in applied mathematics and mechanics",
issn = "1617-7061",
publisher = "Wiley-VCH Verlag",
number = "1",
note = "90th Annual Meeting of the International Association of Applied Mathematics and Mechanics - 2019, 19th GAMM 2019 ; Conference date: 18-02-2019 Through 22-02-2019",
url = "https://jahrestagung.gamm-ev.de/index.php/2019/2019-annual-meeting",

}

RIS

TY - JOUR

T1 - Two-step simulation approach for laser shock peening

AU - Pozdnyakov, Vasily

AU - Keller, Sören

AU - Kashaev, Nikolai

AU - Klusemann, Benjamin

AU - Oberrath, Jens

N1 - Conference code: 90

PY - 2019/11

Y1 - 2019/11

N2 - Laser shock peening (LSP) is a surface modification technique to introduce compressive residual stresses (RS) with a high magnitude in the near surface region of the material. Due to non-linear interactions (e.g. laser absorption by plasma, shock wave propagation, etc.) and a high number of parameters, it is difficult to study and optimize the process based on experiments alone. Therefore, a two-step simulation approach is proposed in this paper, where two models are combined, because one model of the complete process is difficult to derive, due to the different characteristics of the plasma formation and the shockwave propagation in the material. On one hand, a global model including plasma and shock wave descriptions is applied for the LSP of an aluminium sample with water confinement. The numerical solution of this model, applied for a 3×3 mm2focus size, 5 J and 20 ns (full width at half maximum (FWHM)) laser pulse, allows to determine the temporal plasma pressure evolution on the material surface. On the other hand, a finite element simulation is used to calculate the RS distribution within the target material, where the plasma pressure is applied as a surface loading for the aluminium alloy AA2198-T3. The simulated residual stresses are fitted to measurements via parameter variation of the global model. The identified values and the two-step simulation approach can be used in future work to predict stress states of materials after LSP for various processparameters variations.

AB - Laser shock peening (LSP) is a surface modification technique to introduce compressive residual stresses (RS) with a high magnitude in the near surface region of the material. Due to non-linear interactions (e.g. laser absorption by plasma, shock wave propagation, etc.) and a high number of parameters, it is difficult to study and optimize the process based on experiments alone. Therefore, a two-step simulation approach is proposed in this paper, where two models are combined, because one model of the complete process is difficult to derive, due to the different characteristics of the plasma formation and the shockwave propagation in the material. On one hand, a global model including plasma and shock wave descriptions is applied for the LSP of an aluminium sample with water confinement. The numerical solution of this model, applied for a 3×3 mm2focus size, 5 J and 20 ns (full width at half maximum (FWHM)) laser pulse, allows to determine the temporal plasma pressure evolution on the material surface. On the other hand, a finite element simulation is used to calculate the RS distribution within the target material, where the plasma pressure is applied as a surface loading for the aluminium alloy AA2198-T3. The simulated residual stresses are fitted to measurements via parameter variation of the global model. The identified values and the two-step simulation approach can be used in future work to predict stress states of materials after LSP for various processparameters variations.

KW - Engineering

UR - https://www.mendeley.com/catalogue/66a450f8-b741-3bca-8419-f58953c12e3f/

U2 - 10.1002/pamm.201900497

DO - 10.1002/pamm.201900497

M3 - Conference article in journal

VL - 19

JO - Proceedings in applied mathematics and mechanics

JF - Proceedings in applied mathematics and mechanics

SN - 1617-7061

IS - 1

M1 - e201900497

T2 - 90th Annual Meeting of the International Association of Applied Mathematics and Mechanics - 2019

Y2 - 18 February 2019 through 22 February 2019

ER -

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