F
Fei Qin
Researcher at Northwestern Polytechnical University
Publications - 103
Citations - 1551
Fei Qin is an academic researcher from Northwestern Polytechnical University. The author has contributed to research in topics: Combustion & Combustor. The author has an hindex of 17, co-authored 94 publications receiving 951 citations. Previous affiliations of Fei Qin include Lund University.
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Chemical mechanism development and reduction for combustion of NH3/H2/CH4 mixtures
TL;DR: In this article, a detailed chemical model for comprehensive prediction of ammonia/hydrogen/methane mixture combustion was presented. But the model was not suitable for CFD modeling, and the speedup factor was over 5 when using the reduced mechanism with different codes.
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Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor
TL;DR: In this paper, a large eddy simulation (LES) of supersonic turbulent mixing and combustion adopting a partially stirred Reactor (PaSR) sub-grid combustion model is performed for a hydrogen fueled model scramjet combustor.
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Detailed numerical simulation of transient mixing and combustion of premixed methane/air mixtures in a pre-chamber/main-chamber system relevant to internal combustion engines
TL;DR: In this article, a simplified prechamber/main-chamber system is investigated using direct numerical simulation (DNS) with detailed chemical kinetics, and the progress and topology of flame evolution, and mean burning velocity in the main chamber are analyzed in detail.
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Enhanced thermal management with microencapsulated phase change material particles infiltrated in cellular metal foam
TL;DR: In this article, a new strategy for passive thermal management with microencapsulated phase change material (MEPCM) particles embedded into cellular metal foam was proposed in order to improve the thermal conductivity of PCM.
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Simulations of combustion oscillation and flame dynamics in a strut-based supersonic combustor
TL;DR: In this paper, a three-dimensional compressible large eddy simulation was performed on a hydrogen-fueled combustor and pressure fluctuations were recorded, and the analysis of pressure data showed that the combustion processes are intrinsically unstable under supersonic air inflow conditions.