Blown Flaps for Stol Operation: An Examination of the Lift Increment due to the Deflexion of Propeller Slipstream by Large Span Blown Flaps

By Schwartzberg Milton A.  

Aircraft Engineering, Vol. 31, Iss. 10, 1993-12 ,pp. : 308-311

Emerald Group Publishing Ltd

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Fabric in Shear: An Instructive Experiment in Connexion with the Theory of Thin Sheets in Spar Webs

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Aircraft Engineering, Vol. 8, Iss. 8, 1993-12 ,pp. : 227-228

Emerald Group Publishing Ltd

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Information Support for Space Experiments Based on a Numerical-Analytical Theory of Satellite Motion

By Bakhtigaraev N.   Chazov V.  

Cosmic Research, Vol. 43, Iss. 5, 2005-09 ,pp. : 369-372

MAIK Nauka/Interperiodica

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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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Shear Stress in Thin-Walled Tubes: The Theory and Practice of the Calculations Involved, Taking into Account the Effect of Stringers

By B.Sc. C.K. Ovenston  

Aircraft Engineering, Vol. 11, Iss. 11, 1993-12 ,pp. : 417-420

Emerald Group Publishing Ltd

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