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Laminar-Turbulent Transition and Turbulence

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Three-Dimensional Attached Viscous Flow

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Abstract

The state of the boundary layer, laminar or turbulent, influences the drag, the performance of the wing, of stabilization and control devices etc., and the flight characteristics of an airplane. A given flight vehicle is considered as “transition insensitive”, if the location of laminar-turbulent transition does not affect these items.

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Authors and Affiliations

  1. Herzog-Heinrich-Weg 6, 85604, Zorneding, Germany

    Ernst Heinrich Hirschel

  2. 158, rue de Pont Vieux, 31810, Le Vernet, France

    Jean Cousteix

  3. Wilhelm-Evers-Str. 2, 37120, Bovenden, Germany

    Wilhelm Kordulla

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  1. Ernst Heinrich Hirschel
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Hirschel, E.H., Cousteix, J., Kordulla, W. (2014). Laminar-Turbulent Transition and Turbulence. In: Three-Dimensional Attached Viscous Flow. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-41378-0_9

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  • DOI: https://doi.org/10.1007/978-3-642-41378-0_9

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-41377-3

  • Online ISBN: 978-3-642-41378-0

  • eBook Packages: EngineeringEngineering (R0)

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