Computation of Viscous Transonic Flow Around the F5 Wing

Author:

Rizzi Arthur

Publisher

Springer Berlin Heidelberg

Reference30 articles.

1. MacCormack, R.W., ‘The Effect of Viscosity in Hypervelocity Impact Cratering’, AIAA Paper 69–354, 1969.

2. Beam, R.M., and Warming, R.F., ‘An Implicit Factored Scheme for the Compressible Navier-Stokes Equations’, AIAA J., Vol. 16, 1978, pp. 393–402.

3. Jameson, A., Schmidt, W., and Turkel, E., ‘Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes’, AIAA Paper 81–1259, 1981.

4. Rizzi, A., ‘Damped Euler-Equation Method to Compute Transonic Flow Around Wing-Body Combinations’, AIAA J., Vol. 20, 1982, pp. 1321–1328.

5. Haase, W., Wagner, B., and Jameson, A., ‘Development of a Navier-Stokes Method Based on a Finite Volume Technique for the Unsteady Euler Equations’, in ‘Proceedings of the 5th GAMM Conference on Numerical Methods in Fluid Mechanics’, (M. Pandolfi, R. Piva, Eds.), Notes on Num. Fluid Mech., Vol. 7, Vieweg, Braunschweig, 1984, pp. 99–107.

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