An investigation of boundary layer effects on two dimensional supersonic aerofoils

An investigation of boundary layer effects on two dimensional supersonic aerofoils

Zienkiewicz, H. K.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7338
Date: 1951-12

Abstract:

The phenomena of viscous flow over two-dimensional supersonic aerofoils are investigated with a view to developing a method for estimating their effects in the aerodynamic characteristics of the aerofoils. Continues …

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