An investigation of boundary layer effects on two dimensional supersonic aerofoils
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An investigation of boundary layer effects on two dimensional supersonic aerofoils
Zienkiewicz, H. K.
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https://reports.aerade.cranfield.ac.uk/handle/1826.2/4725
Description:
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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CoA. Reports
[280]
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