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Development of Efficient Algorithms for the Solutions of Full Potential and Euler Equations on Vector Computers

  • R. K. Jain
  • N. Kroll
  • R. Radespiel
Part of the Notes on Numerical Fluid Mechanics book series (NNFM, volume 12)

Summary

For the efficient use of vector computers, three problems in the area of computational aerodynamics are dealt with. These are: 3-D full potential equation, body-fitted grid generation for wing-body configurations and 3-D Euler equations. Special features of each of these problems are emphasized. Various techniques to overcome the bottlenecks appearing therein are described.

Keywords

Euler Equation Transonic Flow Large Grid Finite Volume Scheme Vector Computer 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. [1]
    Jameson, A. and Caughey, D.A.: “Numerical calculation of transonic flow past a swept wing”, ERDA Report C00-3077-140, New York Univ. (1977) .Google Scholar
  2. [2]
    Yu, N.J.: “Grid generation and transonic flow calculations for three-dimensional configurations”, AIAA Paper No. 80-1391, (1980) .Google Scholar
  3. [3]
    Radespiel, R. and Kroll, N.: “Progress in the development of an efficient finite volume code for the three dimensional Euler equations”, DFVLR FB 85-31 (1985).Google Scholar
  4. [4]
    Cornelius, H.: Private communication, (1985).Google Scholar
  5. [5]
    Jameson, A., Schmidt, W. and Turkei, E.: “Numerical solutions of the Euler equations by finite volume Methods using Runge-Kutta time-stepping schemes”, AIAA Paper No. 81-1259 (1981).Google Scholar

Copyright information

© Springer Fachmedien Wiesbaden 1986

Authors and Affiliations

  • R. K. Jain
    • 1
  • N. Kroll
    • 1
  • R. Radespiel
    • 1
  1. 1.Institute for Design AerodynamicsDFVLRBraunschweigFed. Rep. Germany

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