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Computer simulation of non-potential flows around wings

Published online by Cambridge University Press:  04 July 2016

Arthur Rizzi
Arthur Rizzi*
Affiliation:
FFAThe Aeronautical Research Institute of Sweden, S-161 11 Bromma, Sweden
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Extract

The Euler equations are proving to be an appropriate model for in viscid vortex flow. This paper demonstrates the range of this model’s applicability by presentation of flowfields computed around a number of different wings with either sharp or rounded edges at transonic and supersonic speeds. The emphasis here is on the physics of the flow model rather than the numerical aspects of the solution method. The results display both expected as well as unexpected vortex phenomena and they indicate the value of this computational tool. Particular attention is paid to the wake regions.

Type
Research Article
Information
The Aeronautical Journal , Volume 88 , Issue 876 , July 1984 , pp. 238 - 248
Copyright
Copyright © Royal Aeronautical Society 1984 

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References

1. Rizzi, A., Eriksson, L. E., Schmidt, W. and Hitzel, S. M. Numerical Solutions of the Euler Equations Simulating Vortex Flows Around Wings, AGARD CP 342, 1983.Google Scholar
2. Jameson, A. and Baker, T. J. Multigrid Solution of the Euler Equations for Aircraft Configurations, AIAA Paper No. 84-0093, New York, 1984.Google Scholar
3. Rizzi, A. Damped Euler-Equations Method to Compute Transonic Flow Around Wing-Body Combinations, AIAA J, October 1982, 20, 1321–1328.Google Scholar
4. Rizzi, A. and Eriksson, L. E. Explicit Multistage Finite Volume Procedure to Solve the Euler Equations for Transonic Flow, and Computational Fluid Dynamics, Lecture Series Notes 1983-04, von Karman Inst., Brussels, 1983.Google Scholar
5. Eriksson, L. E. and Rizzi, A. Computer-Aided Analysis of the Convergence to Steady State of a Discrete Approximation to the Euler Equations, Journal Computational Physics, in press, 1984.Google Scholar
6. Eriksson, L. E. A Study of Mesh Singularities and Their Effects on Numerical Errors, FFA TN 1984-10, Stockholm 1984.Google Scholar
7. Eriksson, L. E. and Rizzi, A. Computation of Vortex Flow Around Wings Using the Euler Equations, ed. Viviand, H., Proc. 4th GAMM Conf. Num. Meth., Braunschweig Vieweg Verlag, 1982.Google Scholar
8. Eriksson, L. E. Practical Three-Dimensional Mesh Generation Using Transfinite Interpolation, Computational Fluid Dynamics, Lecture Series Notes 1983-04, von Karman Inst., Brussels, 1983.Google Scholar