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Application of Generalized Potentials on Plane Transonic Flow

  • H. Sobieczky
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

Summary

The formulation of transonic boundary value problems in a modified hodograph plane is the basis for design methods of plane compressible flow. Rheoelectric analogy and the method of characteristics is used for the design of airfoils.

Keywords

Transonic Flow Sonic Line Transonic Shock Hyperbolic Region Hodograph Method 
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References

  1. 1.
    Busemann, A.: Hodographenmethode der Gasdynamik. Z. angew. Math. Mech. 17 (1937), S. 73–77.MATHCrossRefGoogle Scholar
  2. 2.
    Weinstein, A.: Generalized axially symmetric potential theory. Bull. Amer. Math. Soc. 53 (1953), S. 20–38.CrossRefGoogle Scholar
  3. 3.
    Sobieczky, H.: Exakte Lösungen der ebenen gasdynamischen Gleichungen in Schallnähe. Z. Flugwiss. 19 (1971), S. 197–214.MATHGoogle Scholar
  4. 4.
    Sobieczky, H.: Die abgelöste transsonische Kopfwelle. Z. Flugwiss. 22 (1974), S. 65–73.MATHGoogle Scholar
  5. 5.
    Sobieczky, H.: Entwurf überkritischer Profile mit Hilfe der rheoelektrischen Analogie. DLR-FB 75-43 (1975).Google Scholar

Copyright information

© Springer-Verlag, Berlin/Heidelberg 1976

Authors and Affiliations

  • H. Sobieczky
    • 1
  1. 1.Institut für Strömungsmechanik derDFVLR-AVAGöttingenGermany

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