Senbin Yu

ORCID: 0000-0001-5254-6679
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About
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Research Areas
  • Combustion and flame dynamics
  • Advanced Combustion Engine Technologies
  • Fire dynamics and safety research
  • Combustion and Detonation Processes
  • Surface Roughness and Optical Measurements
  • Advanced Measurement and Metrology Techniques
  • Computational Fluid Dynamics and Aerodynamics
  • Fluid Dynamics and Turbulent Flows
  • Advanced Control Systems Optimization
  • Catalytic Processes in Materials Science
  • Coal Combustion and Slurry Processing
  • Vehicle emissions and performance
  • Advanced Surface Polishing Techniques
  • Radiative Heat Transfer Studies
  • Atmospheric chemistry and aerosols
  • Energetic Materials and Combustion
  • Fuel Cells and Related Materials
  • Industrial Vision Systems and Defect Detection
  • Wind and Air Flow Studies
  • Electric and Hybrid Vehicle Technologies
  • Advanced Power Generation Technologies

Shanghai Research Institute of Sports Science
2024

Lund University
2017-2021

Xi'an Jiaotong University
2014-2015

Imperial College London
2014

National Formosa University
2002-2003

Methane and hydrogen-enriched (25 vol% 50 H2-enriched CH4) methane/air premixed flames were investigated in a gas turbine model combustor under atmospheric conditions. The flame operability ranges mapped at different Reynold numbers (Re), showing the dependence on Re H2 concentrations. effects of equivalence ratio (Φ), Re, enrichment structure examined employing OH-PLIF measurement. For CH4/air cases, was stabilized with an M shape; while for transitions to П shape above specific Φ. This...

10.1016/j.ijhydene.2021.01.087 article EN cc-by International Journal of Hydrogen Energy 2021-02-10

An experimental and numerical study on thermal chemical effects of water vapor addition the laminar burning velocities syngas was conducted using a constant-volume chamber CHEMKIN package. The conditions in present for CO/H2/air/H2O mixtures with hydrogen fraction were from 5% to 50%, initial temperature 373 K, pressures 0.1 0.5 MPa dilution ratios 0% 30%. measured velocity data compared simulations three mechanisms, San Diego mechanism those Davis et al. Li showed reasonable agreement...

10.1021/ef4020586 article EN Energy & Fuels 2014-04-14

Large-eddy simulation with a finite-rate chemistry model is carried out to investigate the formation of soot and nitrogen oxides (NOx) in dual-fuel spray combustion. Liquid n-heptane injected into constant volume chamber, filled premixed methanol–air mixture an equivalence ratio (ϕm) 0.3. Three cases are simulated under initial temperatures 900, 950 1000 K. single-fuel cases, same configurations, but pure air being used as ambient gas composition also baselines for comparison purposes. The...

10.1016/j.apenergy.2020.115774 article EN cc-by Applied Energy 2020-09-06

10.1007/s001700200038 article EN The International Journal of Advanced Manufacturing Technology 2002-02-26

10.1016/j.proci.2014.06.044 article EN Proceedings of the Combustion Institute 2014-07-08

Experimental and numerical studies were performed to understand the stabilization of lean premixed natural gas/air flames in a gas turbine model combustor which was equipped with swirl burner, known as CECOST designed replicate flow flame structures an industrial engine. The operability range, stabilization, flashback investigated employing simultaneous OH– CH2O-PLIF, high-speed chemiluminescence imaging. Large eddy simulation (LES) carried out for analysis vortex breakdown under...

10.1016/j.fuel.2020.118421 article EN cc-by Fuel 2020-07-07

Clean technology has become a key feature due to increasing environmental concerns. Swirling flows, being directly associated with combustion performance and hence minimized pollutant formation, are encountered in most propulsion power-generation devices. In this study, the development process of conceptual swirl burner developed at Swedish National Centre for Combustion Technology (CeCOST), is presented. Utilizing extensive computational fluid dynamics (CFD) analysis, both lead time cost...

10.1115/gt2018-75760 article EN 2018-06-11

In a piloted jet flame, the pilot flame has an effect of stabilizing main flame. Detailed mechanisms flame/main interaction are however not well studied. It is expected that affects through following mechanisms: (a) provides heat and radicals to reaction zone (b) prevents cold ambient air from being entrained into (c) modifies stretch rate this paper, detailed numerical simulations laminar methane/air flames carried out elucidate on structure burning velocity One-dimensional (1D) freely...

10.1080/00102202.2019.1679550 article EN cc-by-nc-nd Combustion Science and Technology 2019-10-23
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