Computation of unsteady flow and aerodynamic noise of NACA0018 airfoil using large-eddy simulation

International Journal of Heat and Fluid Flow

Volumn 27, Issue 2, 2006, Pages 229-242

  Kim, H J ^a   Lee, S ^a   Fujisawa, N ^b  

^a Inha University   (South Korea)

^b NIIGATA UNIVERSITY   (Japan)

Author keywords

Aero acoustics; Discrete tone noise; LES; Subgrid scale model

Indexed keywords

ACOUSTIC NOISE; AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; LAMINAR FLOW; MATHEMATICAL MODELS; UNSTEADY FLOW; VORTEX FLOW; VORTEX SHEDDING;

AERO-ACOUSTICS; DISCRETE TONE NOISE; LARGE EDDY SIMULATION; SUBGRID-SCALE MODEL;

AIRFOILS;

ACOUSTIC NOISE; AERODYNAMICS; AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; LAMINAR FLOW; MATHEMATICAL MODELS; UNSTEADY FLOW; VORTEX FLOW; VORTEX SHEDDING;

EID: 32944476350     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijheatfluidflow.2005.08.007     Document Type: Article

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