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An Exact Hodographmethod for the Design of Supercritical Wingsections

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Summary

This contribution describes a simple hodographmethod for the design of transonic airfoils mainly based on Sobieczky’s rheographtransformation. A classical panelmethod solves the elliptic part of the flow problem, whereas a method of characteristics is applied for the treatment of the inbedded supersonic region.

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References

  1. Sobieczky, H.: Analog-analytische Konstruktion überkritischer Profilströmungen. DGLR Nr. 72-129 (1972)

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  2. Sobieczky, H.: Entwurf überkritischer Profile mit Hilfe der rheoelektrischen Analogie. DLR 75-43 (1975)

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  3. Eberle, A.: Transsonischer Profilentwurf MBB UFE 1108-74 ö (1974)

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  4. Eberle, A.: Eine exakte Hodographenmethode zum Entwurf überkritischer Profile. MBB UFE 1168-75 ö (1975)

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© 1976 Springer-Verlag, Berlin/Heidelberg

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Eberle, A. (1976). An Exact Hodographmethod for the Design of Supercritical Wingsections. In: Oswatitsch, K., Rues, D. (eds) Symposium Transsonicum II. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_35

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  • DOI: https://doi.org/10.1007/978-3-642-81005-3_35

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-81007-7

  • Online ISBN: 978-3-642-81005-3

  • eBook Packages: Springer Book Archive

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