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Part of the book series: Progress in Scientific Computing ((PSC,volume 6))

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Abstract

In the early 1970’s Murman and Cole in a landmark paper [1] set the groundwork for the development of computational fluid dynamics for years to come. Their paper demonstrated the use of type dependent finite difference approximations, chosen according to the characteristic speeds of the flow, and Gauss-Seidel line relaxation to solve the transonic small disturbance equation. Following their success, Jameson [2] introduced a “rotated” difference scheme and extended the Murman-Cole procedure to solve the full potential equation. These early contributions were responsible for the rapid growth and widespread application of computational fluid dynamics to aerodynamic design in the 1970’s. Last year Chakravarthy [3] applied flux-split type-dependent difference approximations and Gauss-Seidel line relaxation to solve the Euler equations. And this year Napolitano and Walters [4] and this author [5] used these procedures to solve the Navier-Stokes equations. On the one hand it’s amazing that the same key features of the Murman-Cole scheme can be applied to the more complete sets of governing equations, and on the other it’s amazing that it took a decade and a half to realize it. This paper outlines the use of these features for solving the Navier-Stokes equations and presents some computed results demonstrating high numerical efficiency.

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References

  1. Murman, E. M. and Cole, J.D., “Calculation of Plane Steady Transonic Flows,” AIAA Journal, Vol. 9 No. 1, January 1971, pp 114–121.

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  2. Jameson, A., “Numerical Calculation of the Three Dimensional Tran- sonic Flow Over a Yawed Wing.” Proceedings, A.AA Computational Fluid Dynamics Conference, Palm Springs, CA, July 19–20, 1973.

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  3. Chakravarthy, S. R., “Relaxation Metllods for Unfactored Implicit Upwind Schemes,” AIAA Paper No. 84–0165, 1984.

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  4. Napolitano, M. and Walters, R. W., “An Incremental Block-Line Gauss-Seidel Method for the Navier-Stokes Equations” AIAA Paper No. 85–0033, 1985.

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  5. IacCormack, R. W., “Current Status of Numerical Solutions of the Navier-Stokes Equations,” AIAA Paper No. 85–0032, 1985.

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  6. Steger, J. and Warming, R. F., “Flux Vector Splitting of the Inviscid Gasdynamics Equations with Application to Finite Difference Methods,” NASA TM-78605, 1979.

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  7. MacCormack, R. W., “The Effect of Viscosity in Hypervelocity Impact Cratering,” AIAA Paper No. 69–354, 1969.

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  8. Mason, M. L., Putnam, L. E. and Re, R. J., “The Effect of Throat Contouring on Two-Dimensional Converging-Diverging Nozzles at Sonic Conditions,” NASA Technical Paper 1704, 1980.

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  9. Kneile, K. R. and MacCormack, R. W., “Implicit Solution of the 3-D Compressible Navier-Stokes Equations for Internal Flows,” Proceedings of the 9th International Conference on Numerical Methods in Fluid Dynamics, Saclay, France, 1984.

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© 1985 Birkhäuser Boston, Inc.

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MacCormack, R.W. (1985). Numerical Methods for the Navier-Stokes Equations. In: Murman, E.M., Abarbanel, S.S. (eds) Progress and Supercomputing in Computational Fluid Dynamics. Progress in Scientific Computing, vol 6. Birkhäuser Boston. https://doi.org/10.1007/978-1-4612-5162-0_8

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  • DOI: https://doi.org/10.1007/978-1-4612-5162-0_8

  • Publisher Name: Birkhäuser Boston

  • Print ISBN: 978-1-4612-9591-4

  • Online ISBN: 978-1-4612-5162-0

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