Smooth Air Inlet and Maximum Lift Conditions for a Cascade of Thin Aerofoils: An Analysis Based on Schlichting's Cascade Theory Showing that for Shock-Free Inlet Conditions the Angle of Attack must be Zero and that a Symmetrical Camber Line yields the Maximum Lift Coefficient

Author： M.Sc.(Eng.) J.A. Wannenburg   M.Sc.  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.35, Iss.10, 1993-12, pp. : 302-306

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