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Leading edge shape for flat plate boundary layer studies

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Summary

In experimental boundary layer studies, a flat plate with some shaped nose piece is generally used; this is often prone to flow separation at the junction. By analysing the development of a laminar boundary layer on a two-parameter family of nose shapes, it is found that a cubic super-ellipse of axis ratio 6 or higher is a reasonable optimum shape for avoiding separation on or due to such nose-pieces.

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References

  • Curle N (1962) Laminar boundary layer equations. Oxford: Clarendon Press

    Google Scholar 

  • Hess JL; Smith AMO (1968) Calculation of potential flow about arbitrary bodies. Frog Aero Sci 8: 1–138

    Google Scholar 

  • Narasimha R; Prasad SN (1984) Leading edge shape for flat plate boundary layer studies. Fluid Mechanics Rep. 84 FM 3, Dept. Aerospace Engineering, Indian Institute of Science, Bangalore

    Google Scholar 

  • Narasimha R; Devasia KJ; Gururani G; Badri Narayanan MA (1984) Transitional intermittency in boundary layers subjected to pressure gradient. Exp Fluids 2: 171–176

    Google Scholar 

  • Thwaites B (1949) Approximate calculation of the laminar boundary layer. Aero Q 1: 245–280

    Google Scholar 

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Narasimha, R., Prasad, S.N. Leading edge shape for flat plate boundary layer studies. Experiments in Fluids 17, 358–360 (1994). https://doi.org/10.1007/BF01874418

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  • DOI: https://doi.org/10.1007/BF01874418

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