Skip to main content

Numerical calculation of transonic flow past a swept wing by a finite volume method

  • Aeronautical Fluid Mechanics and Transonic Flows
  • Conference paper
  • First Online:
Computing Methods in Applied Sciences and Engineering, 1977, II

Part of the book series: Lecture Notes in Physics ((LNP,volume 91))

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Jameson, Antony: Three dimensional flows acround airfoils with shocks, IFIP Symposium on Computing Methods in Applied Sciences and Engineering, Versailles, December 1973.

    Google Scholar 

  2. Jameson, Antony, and Caughey, D. A.; Numerical calculation of the flow past a swept wing, New York University Report COO-3077-140, June 1977.

    Google Scholar 

  3. Murman, E. M., and Cole, J. D.; Calculation of plane steady transonic flows, AIAA Journal, Vol. 9, 1971, pp. 114–121.

    Google Scholar 

  4. Jameson, Antony; Iterative solution of transonic flows over airfoils and wings, including flows at Mach 1, Comm. Pure Appl. Math., Vol. 27, 1974, pp. 283–309.

    Google Scholar 

  5. Bateman, H.; Notes on a differential equation which occurs in the two dimensional motion of a fluid and the associated variational problem, Proc. Roy. Soc., Series A,, Vol. 125, 1929, pp. 593–613.

    Google Scholar 

  6. Lax, Peter,and Wendroff, Burton; Systems of conservation laws, Comm. Pure Appl. Math., Vol. 13, 1960, pp. 217–237.

    Google Scholar 

  7. Glowinski, R., and Pironneau, O.; On the computation of transonic flows, Premier Colloque Franco-Japonais d'Analyse Fonctionelle et d'Analyse Numerique, Kyoto, September 1976.

    Google Scholar 

  8. Steger, J. L., and Baldwin, B. S.; Shock waves and drag in the numerical calculation of isentropic transonic flow, NASA TN D-6997, 1972.

    Google Scholar 

  9. Klunker, E. B., Contribution to methods for calculating the flow about thin lifting wings at transonic speeds — analytic expressions for the far field, NASA TN D6530, 1971.

    Google Scholar 

  10. Synge, J. L., and Schild, A., Tensor Calculus, University of Toronto Press, 1949, pp. 57–58.

    Google Scholar 

  11. Jameson, Antony, and Caughey, D. A.; A finite volume method for transonic potential flow calculations, Third AIAA Conference on Computational Fluid Dynamics, Albuquerque, June 1977.

    Google Scholar 

  12. Caughey, D. A., and Jameson, Antony, Numerical calculation of transonic potential flow about wing fuselage combinations, AIAA Paper 77-677, AIAA Conference on Plasma an Fluid Dynamics, Albuquerque, June 1977.

    Google Scholar 

  13. Monnerie, B., and Charpin, F., Essais de buffeting d'une aile en fleche en transsonique, 10e Colloque d'Aerodynamique Appliquee, Lille, November 1973.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

R. Glowinski J. L. Lions

Rights and permissions

Reprints and permissions

Copyright information

© 1979 Springer-Verlag

About this paper

Cite this paper

Jameson, A. (1979). Numerical calculation of transonic flow past a swept wing by a finite volume method. In: Glowinski, R., Lions, J.L. (eds) Computing Methods in Applied Sciences and Engineering, 1977, II. Lecture Notes in Physics, vol 91. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-09119-X_97

Download citation

  • DOI: https://doi.org/10.1007/3-540-09119-X_97

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-09119-6

  • Online ISBN: 978-3-540-35512-0

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics