N. Li

ORCID: 0009-0001-9928-1011
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About
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Research Areas
  • Fluid Dynamics and Turbulent Flows
  • Aerodynamics and Acoustics in Jet Flows
  • Combustion and flame dynamics
  • Advanced Combustion Engine Technologies
  • Wind and Air Flow Studies
  • Computational Fluid Dynamics and Aerodynamics
  • Atmospheric chemistry and aerosols
  • Heat Transfer Mechanisms
  • Turbomachinery Performance and Optimization
  • Meteorological Phenomena and Simulations
  • Fluid Dynamics and Vibration Analysis

Qingdao University of Science and Technology
2023-2024

Imperial College London
2004-2009

University of Maryland, College Park
2000

The paper examines, by means of highly resolved large-eddy simulations, the fluid mechanic behaviour an incompressible, turbulent flow separating from axisymmetric, hill-shaped obstacle. hill is subjected to a flat-plate boundary layer thickness half height, developing within large duct in which placed. Reynolds number based on height and free-stream velocity 130000, momentum-thickness 7300. Extensive detailed experimental data are available for these same conditions, compared with...

10.1017/s0022112008005661 article EN Journal of Fluid Mechanics 2009-05-12

A method to generate inflow boundary conditions for large-eddy simulations (LES) of turbulent free shear layers is presented. time series instantaneous velocity planes, with duration approximately equal the integral scale flow, extracted from a periodic simulation and saved on disk. This signal transformed into one, by using conventional windowing technique, re-used in actual as many times required obtain converged statistics. The applied LES spatially developing mixing layer. It shown that...

10.1063/1.870346 article EN Physics of Fluids 2000-04-01

Abstract The paper investigates, by means of a simulation methodology, the flow separating from 40 degrees backward-swept wing at 9 incidence and Reynolds number 210,000, based on wing-root chord length. Simulation corresponds to LDA, PIV suction-side-topology measurements for same geometry, conducted other investigators specifically provide validation data. finest block-structured mesh contains 23·6 million nodes is organised in 256 blocks maximise quality facilitate parallel solution...

10.1017/s0001924000004863 article EN The Aeronautical Journal 2007-11-01

Given unsteady operating conditions, the combustion process in gas turbine combustor often suffers from equivalence ratio fluctuations (ERFs), which induce instability. In this study, effects of ERFs on a swirl-stabilized premixed flame were studied by large eddy simulation (LES). A new model with turbulence modification and two-step methane oxidation mechanism employed to simulate interaction between chemical reactions. LES was first validated comparing results corresponding experimental...

10.1080/15567036.2023.2227137 article EN Energy Sources Part A Recovery Utilization and Environmental Effects 2023-06-26
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