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  1. No Access

    Chapter and Conference Paper

    A Hybrid LES/CAA Method for Aeroacoustic Applications

    This paper describes a hybrid LES/CAA approach for the numerical prediction of airframe and combustion noise. In the hybrid method first a Large-Eddy Simulation (LES) of the flow field containing the acoustic ...

    Qinyin Zhang, Phong Bui, Wageeh A. El-Askary… in High Performance Computing on Vector Syste… (2006)

  2. No Access

    Chapter and Conference Paper

    Large-Eddy Simulation of Attached Airfoil Flow

    A Large-eddy simulation version of the FLOWer code is introduced to compute attached flow around a quasi three-dimensional airfoil at a Mach number Ma = 0.088, Reynolds number Re = 8 × 105, and an angle of attack...

    Qinyin Zhang, Matthias Meinke… in MEGAFLOW - Numerical Flow Simulation for A… (2005)