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

By M.Sc.(Eng.) J.A. Wannenburg   M.Sc.  

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

Emerald Group Publishing Ltd

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An Investigation of the Lift Produced by a Fan in a Two-Dimensional Wing

By Norland Sven-Anders  

Journal of the American Helicopter Society, Vol. 7, Iss. 4, 1962-10 ,pp. : 25-32

AHS International

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Calculation of Wing Profile Drag: A New Simplified Method of Practical Value to Engineers

By B.Sc Maurice Holt  

Aircraft Engineering, Vol. 15, Iss. 10, 1993-12 ,pp. : 278-280

Emerald Group Publishing Ltd

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The C.P. Position of Aerofoils: A Simple Graphical Method for the Use of the Practical Designer

By Novickis Georges  

Aircraft Engineering, Vol. 10, Iss. 8, 1993-12 ,pp. : 250-250

Emerald Group Publishing Ltd

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Effect of Structural Damping on Panel Flutter: Stability of Two-Dimensional Simply-Supported Panels Using Linear Piston Theory

By M.I.A.S. D.J. Johns   M.Sc.   B.A. P.C. Parks  

Aircraft Engineering, Vol. 32, Iss. 10, 1993-12 ,pp. : 304-308

Emerald Group Publishing Ltd

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