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about LES/RANS hybrid methodology
current research focus
past major research
computational study of a supersonic base flow with LES/RANS hybrid methodology
analysis and prediction of thin-airfoil stall phenomena with LES/RANS hybrid methodology
numerical analysis of pulse detonation engine cycles

method: numerical schemes and modelings


governing equations
  Favre-filtered &Favre-averaged compressible Navier-Stokes equations.
numerical scheme for convective and viscous terms
  6th-order compact difference scheme + 6th-order filtering schme
time integration scheme
  LU-SGS implicit scheme with 2nd-order inner iterations
turbulence modeling
  LES/RANS hybrid methodology
  LES-level turbulence model: Smagorinsky model
  RANS-level turbulence model: Baldwin-Lomax model
flow condition
  M=0.17, Re=uD/ν=5.8x10**6
angles of attack: 4.0-11.0 degs.
   
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