Semidirect solution to steady transonic flow by Newton's method

  • Arthur Rizzi
  • Gunilla Sköllermo
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 141)


Shock Wave Strong Shock Entropy Condition Transonic Flow Finite Difference Solution 
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  1. Baker, T. 1980. Personal communication.Google Scholar
  2. Blomster, J., and Sköllermo, G. 1977. Finite difference computation of steady transonic nozzle flow. Computer Science Dept. Rep. No. 66, Uppsala Univ.Google Scholar
  3. Engquist, B., and Osher, S. 1980. Stable and entropy satisfying approximations for transonic flow calculations. Math. Comp. 34:45–75.Google Scholar
  4. Henrici, P. 1962. Discrete Variable Methods in Ordinary Differential Equations. New York: John Wiley. pp. 364 ff.Google Scholar
  5. Lax, P. 1973. Hyperbolic Systems of Conservation Laws and the Mathematical Theory of Shock Waves. Philadelphia: SIAM.Google Scholar
  6. Martin, E.D., and Lomax, H. 1975. Rapid finite-difference computation of subsonic and slightly supercritical aerodynamic flows. AIAA J. 13: 579–586.Google Scholar

Copyright information

© Springer-Verlag 1989

Authors and Affiliations

  • Arthur Rizzi
    • 1
  • Gunilla Sköllermo
    • 2
  1. 1.FFA The Aeronautical ResearchInstitute of SwedenBrommaSweden
  2. 2.Stockholms Computing CenterStockholmSweden

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