One of the key challenges for accurate prediction of hypersonic aerodynamic heating is the exothermic uncertainty due to the complex surface catalytic recombination effect, which is caused by the strong interactions between highly non-equilibrium dissociated gas and the thermal protection material surface. Employing engineered surface morphology to improve thermal protection effects has been proposed, but its effects on surface catalytic recombination remain unclear. To address this problem, this work employs the reactive molecular dynamics method to investigate the surface adsorption and recombination characteristics of continuous impingement of atomic oxygen upon eight different nano-structured silica surfaces. A parametric study of the influences of the gas incident angles and the surface structural parameters, i.e., roughness factor and surface fraction, is conducted. The results show that the surface catalytic recombination performance is very sensitive to the incident angle of the incoming gas, and the presence of nanostructures increases the recombination rate. The influence of surface morphology shows a complicated feature, where nanostructures with moderated fin height and high surface fraction are beneficial for the inhibition of surface recombination effects, leading to reduced exothermic heat release. Such microscopic revelation of the surface morphology effect is helpful for accurate prediction of aerodynamic heat and provides guidance for the surface engineering of optimized morphology to achieve improved thermal protection effect.
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April 2023
Research Article|
April 14 2023
Influence of surface nanostructures on the catalytic recombination of hyperthermal non-equilibrium flow
Special Collection:
Hypersonic Flow
He Lichao (贺立超)
;
He Lichao (贺立超)
(Data curation, Formal analysis, Investigation, Methodology, Validation, Visualization, Writing – original draft)
1
School of Aeronautic Science and Engineering, Beihang University
, Beijing 100191, China
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Ye Zhifan (叶致凡);
Ye Zhifan (叶致凡)
(Data curation, Investigation, Methodology, Validation, Visualization)
1
School of Aeronautic Science and Engineering, Beihang University
, Beijing 100191, China
2
Institute of Thermodynamics, Technical University of Munich
, Munich 80333, Germany
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Cao Yingfei (曹盈菲)
;
Cao Yingfei (曹盈菲)
(Investigation, Methodology, Validation, Visualization)
3
Sino-French Engineer School/School of General Engineering, Beihang University
, Beijing 100191, China
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Tang Ju (汤巨)
;
Tang Ju (汤巨)
(Investigation, Methodology, Validation, Visualization)
3
Sino-French Engineer School/School of General Engineering, Beihang University
, Beijing 100191, China
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Zhao Jin (赵瑾)
;
Zhao Jin (赵瑾)
a)
(Conceptualization, Funding acquisition, Methodology, Project administration, Supervision, Writing – original draft, Writing – review & editing)
1
School of Aeronautic Science and Engineering, Beihang University
, Beijing 100191, China
2
Institute of Thermodynamics, Technical University of Munich
, Munich 80333, Germany
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Wen Dongsheng (文东升)
Wen Dongsheng (文东升)
a)
(Conceptualization, Funding acquisition, Project administration, Supervision, Writing – review & editing)
1
School of Aeronautic Science and Engineering, Beihang University
, Beijing 100191, China
2
Institute of Thermodynamics, Technical University of Munich
, Munich 80333, Germany
3
Sino-French Engineer School/School of General Engineering, Beihang University
, Beijing 100191, China
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Note: This paper is part of the special topic, Hypersonic Flow.
Physics of Fluids 35, 042108 (2023)
Article history
Received:
February 09 2023
Accepted:
March 27 2023
Citation
Lichao He, Zhifan Ye, Yingfei Cao, Ju Tang, Jin Zhao, Dongsheng Wen; Influence of surface nanostructures on the catalytic recombination of hyperthermal non-equilibrium flow. Physics of Fluids 1 April 2023; 35 (4): 042108. https://doi.org/10.1063/5.0145963
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