论文信息 - Implicit Central Difference Simulation of Compressible Navier-Stokes Flow Over a NACA0012 Airfoil - 字舞流文

Implicit Central Difference Simulation of Compressible Navier-Stokes Flow Over a NACA0012 Airfoil

Transonic laminar flow at low Reynolds numbers over a NACA0012 airfoil is numerically simulated by solving the two-dimensional compressible Navier-Stokes equations by means of the implicit central difference scheme of Beam and Warming.

B. Müller | A. Rizzi | T. Berglind | A. Rizzi | B. Müller | T. Berglind

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