Summary
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.
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References
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© 1987 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig
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Müller, B., Berglind, T., Rizzi, A. (1987). Implicit Central Difference Simulation of Compressible Navier-Stokes Flow Over a NACA0012 Airfoil. In: Bristeau, M.O., Glowinski, R., Periaux, J., Viviand, H. (eds) Numerical Simulation of Compressible Navier-Stokes Flows. Notes on Numerical Fluid Mechanics, vol 18. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-87873-1_11
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DOI: https://doi.org/10.1007/978-3-322-87873-1_11
Publisher Name: Vieweg+Teubner Verlag
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