Cooling of a laser-modified surface with a dispersed flow of coolant

The paper deals with the study of heat transfer intensification during cooling of a surface treated by laser with a dispersed coolant flow. A laser ablation technique using a pulsed laser is described; this treatment leads to the formation of craters of up to 600 µm in diameter on a copper surface with the following roughness parameters: R a = 1.48 µm, R z = 9.8 µm. The results demonstrate an increase in the removed heat flux by 35–40 %, the heat transfer coefficient by 38–55 % at intense boiling (115–125 °C) compared to the unmodified surface. The proportion of heat removed due to the phase transition reaches 90 % at a removed heat flux density of 8.4 MW/m 2 on the modified surface.

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Publication Details

Journal
Thermophysics and Aeromechanics
Published
2026-07-25
DOI
https://doi.org/10.1134/s0869864326010051
Primary Topic
Heat Transfer Mechanisms
Type
article
Field-Weighted Citation Impact
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article

Cooling of a laser-modified surface with a dispersed flow of coolant

В. С. Штелинг, P.P. Shcherbakov, A. T. Komov, А.С. Филаков et al.
Thermophysics and Aeromechanics
Heat Transfer Mechanisms
article

Cooling of a laser-modified surface with a dispersed flow of coolant

В. С. Штелинг, P.P. Shcherbakov, A. T. Komov, А.С. Филаков, A. V. Zakharchenkov
article en

Abstract

The paper deals with the study of heat transfer intensification during cooling of a surface treated by laser with a dispersed coolant flow. A laser ablation technique using a pulsed laser is described; this treatment leads to the formation of craters of up to 600 µm in diameter on a copper surface with the following roughness parameters: R a = 1.48 µm, R z = 9.8 µm. The results demonstrate an increase in the removed heat flux by 35–40 %, the heat transfer coefficient by 38–55 % at intense boiling (115–125 °C) compared to the unmodified surface. The proportion of heat removed due to the phase transition reaches 90 % at a removed heat flux density of 8.4 MW/m 2 on the modified surface.

Thermophysics and AeromechanicsVol. 33(1)
Moscow Power Engineering Institute (RU)
Openalex Percentile: Top 16%
Heat Transfer Mechanisms
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