Heat Transfer and Mode Transition for Laser Ablation Subjected to Supersonic Airflow
When laser ablation is subjected to supersonic flow, the influence mechanism of airflow on laser ablation behavior is still unclear. A coupled thermal-fluid-structure model is presented to investigate the influence of supersonic airflow on the development of a laser ablation pit. Results show that t...
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| Published in | Chinese physics letters Vol. 33; no. 1; pp. 44 - 47 |
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| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
2016
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| Subjects | |
| Online Access | Get full text |
| ISSN | 0256-307X 1741-3540 |
| DOI | 10.1088/0256-307X/33/1/014201 |
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| Abstract | When laser ablation is subjected to supersonic flow, the influence mechanism of airflow on laser ablation behavior is still unclear. A coupled thermal-fluid-structure model is presented to investigate the influence of supersonic airflow on the development of a laser ablation pit. Results show that the aerodynamic convection cooling effect not only reduces the ablation velocity but also changes the symmetry morphology of the ablation pit due to the non-uniform convective heat transfer. Flow mode transition is also observed when the pit becomes deeper, and significant change in flow pattern and heat transfer behavior are found when the open mode is transformed into the closed mode. |
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| AbstractList | When laser ablation is subjected to supersonic flow, the influence mechanism of airflow on laser ablation behavior is still unclear. A coupled thermal-fluid-structure model is presented to investigate the influence of supersonic airflow on the development of a laser ablation pit. Results show that the aerodynamic convection cooling effect not only reduces the ablation velocity but also changes the symmetry morphology of the ablation pit due to the non-uniform convective heat transfer. Flow mode transition is also observed when the pit becomes deeper, and significant change in flow pattern and heat transfer behavior are found when the open mode is transformed into the closed mode. |
| Author | 黄亿辉 宋宏伟 黄晨光 |
| AuthorAffiliation | Key Laboratory for Mechanics in Fluid-Solid Coupling Systems, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190 |
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| CitedBy_id | crossref_primary_10_1016_j_compstruct_2018_03_031 crossref_primary_10_2139_ssrn_4118449 crossref_primary_10_1016_j_ceramint_2020_06_115 crossref_primary_10_1016_j_ijthermalsci_2021_107414 crossref_primary_10_1016_j_taml_2018_04_003 crossref_primary_10_1016_j_ijthermalsci_2024_109230 crossref_primary_10_1016_j_compstruct_2022_116139 crossref_primary_10_1016_j_ijthermalsci_2023_108174 |
| Cites_doi | 10.3788/HPLPB20112304.0866 10.1007/s00339-011-6702-8 10.1016/S0143-8166(01)00008-2 10.1016/j.jmaa.2010.12.039 10.1016/S0030-3992(01)00048-2 10.3788/HPLPB20132509.2229 10.3788/HPLPB20102206.1215 10.1016/j.optlaseng.2008.05.010 10.1115/1.1510518 10.1007/s10853-005-6118-y |
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| Notes | 11-1959/O4 When laser ablation is subjected to supersonic flow, the influence mechanism of airflow on laser ablation behavior is still unclear. A coupled thermal-fluid-structure model is presented to investigate the influence of supersonic airflow on the development of a laser ablation pit. Results show that the aerodynamic convection cooling effect not only reduces the ablation velocity but also changes the symmetry morphology of the ablation pit due to the non-uniform convective heat transfer. Flow mode transition is also observed when the pit becomes deeper, and significant change in flow pattern and heat transfer behavior are found when the open mode is transformed into the closed mode. Yi-Hui Huang, Hong-Wei Song, Chen-Guang Huang（Key Laboratory for Mechanics in Fluid-Solid Coupling Systems, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190） ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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| References | 11 12 13 14 Jia H N (4) 2013; 30 16 17 18 Khersonsky A (3) 2000; 4 Matsuda J (5) 1998; 7 Wang W P (7) 2001; 21 Zhao J H (6) 1996; 10 Selin A (19) 1 2 Yuan H (8) 2005; 15 Chung K M (20) Zhang J (15) 2007; 19 Wang Z Y (9) 2000; 21 10 |
| References_xml | – volume: 10 start-page: 262 issn: 1000-5773 year: 1996 ident: 6 publication-title: Chin. J. High Press. Phys. – volume: 21 start-page: 44 year: 2000 ident: 9 publication-title: Laser J. – ident: 16 doi: 10.3788/HPLPB20112304.0866 – volume: 7 start-page: 12 year: 1998 ident: 5 publication-title: Joining Mater. – start-page: 1909 ident: 20 publication-title: 5th AIAA/CEAS Aeroacoustics Conference and Exhibition – ident: 1 doi: 10.1007/s00339-011-6702-8 – ident: 11 doi: 10.1016/S0143-8166(01)00008-2 – volume: 15 start-page: 681 issn: 1001-4322 year: 2005 ident: 8 publication-title: High Power Laser Part. Beams – ident: 17 doi: 10.1016/j.jmaa.2010.12.039 – volume: 30 issn: 0256-307X year: 2013 ident: 4 publication-title: Chin. Phys. Lett. – ident: 12 doi: 10.1016/S0030-3992(01)00048-2 – ident: 10 doi: 10.3788/HPLPB20132509.2229 – volume: 19 start-page: 1818 issn: 1001-4322 year: 2007 ident: 15 publication-title: High Power Laser Part. Beams – ident: 18 doi: 10.3788/HPLPB20102206.1215 – ident: 14 doi: 10.1016/j.optlaseng.2008.05.010 – ident: 13 doi: 10.1115/1.1510518 – volume: 21 start-page: 319 year: 2001 ident: 7 publication-title: Appl. Laser – volume: 4 start-page: 2 year: 2000 ident: 3 publication-title: Adv. Mater. Proce. – start-page: 848 ident: 19 publication-title: The 43rd AIAA Aerospace Sciences Meeting and Exhibition – ident: 2 doi: 10.1007/s10853-005-6118-y |
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| SubjectTerms | Ablation Airflow Heat transfer Joining Laser ablation Supersonic aircraft Supersonic flow Symmetry 对流换热 流动模式 激光烧蚀 烧蚀特性 热传递 结构模型 超声速气流 超音速气流 |
| Title | Heat Transfer and Mode Transition for Laser Ablation Subjected to Supersonic Airflow |
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