Abstract
The positive pressure gradient, downstream of the suction peak at the leading edge of an airfoil at incidence, may, under some conditions, induce large perturbations on the general pattern of the flow.
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© 1984 Springer Science+Business Media New York
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Gleyzes, C., Cousteix, J., Bonnet, J.L. (1984). A Calculation Method of Leading-Edge Separation Bubbles. In: Cebeci, T. (eds) Numerical and Physical Aspects of Aerodynamic Flows II. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-09014-5_10
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DOI: https://doi.org/10.1007/978-3-662-09014-5_10
Publisher Name: Springer, Berlin, Heidelberg
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