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Transitional Spot Formation Rate in Two-Dimensional Boundary Layers

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Numerical and Physical Aspects of Aerodynamic Flows III

Abstract

In two-dimensional constant pressure flows, the distribution of transitional intermittency is [226]

$$\gamma = \left\{ {\begin{array}{*{20}{c}} {1 - \exp \left[ { - \frac{{{{\left( {x - {x_t}} \right)}^2}n\sigma }}{U}} \right]ifx > {x_t}} \\ {0,ifx > {x_t}} \end{array}} \right\}$$
((1.1))

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Author information

Authors and Affiliations

  1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore, 560012, India

    R. Narasimha

  2. National Aeronautical Laboratory, Bangalore, 560017, India

    R. Narasimha

  3. Department of Mechanical Engineering, Indian Institute of Science, Bangalore, 560012, India

    J. Dey

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  1. R. Narasimha
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  2. J. Dey
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Editor information

Editors and Affiliations

  1. Douglas Aircraft Company, Long Beach, CA, 90846, USA

    Tuncer Cebeci

  2. California State University, Long Beach, CA, 90840, USA

    Tuncer Cebeci

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© 1986 Springer-Verlag New York Inc.

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Narasimha, R., Dey, J. (1986). Transitional Spot Formation Rate in Two-Dimensional Boundary Layers. In: Cebeci, T. (eds) Numerical and Physical Aspects of Aerodynamic Flows III. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-4926-9_4

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  • DOI: https://doi.org/10.1007/978-1-4612-4926-9_4

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-1-4612-9362-0

  • Online ISBN: 978-1-4612-4926-9

  • eBook Packages: Springer Book Archive

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