Electrical Analogue to a Celled Tube Subjected to Flexure and Torsion: A Method of Solution Without Formulating the Structural Equations

By Zaid Melvin   Ryder Frederick L.  

Aircraft Engineering, Vol. 31, Iss. 4, 1993-12 ,pp. : 94-100

Emerald Group Publishing Ltd

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Torsion and Flexure: The Reasons Underlying the Solution of Two Design Problems

By B.Sc. C. Gurney  

Aircraft Engineering, Vol. 11, Iss. 12, 1993-12 ,pp. : 437-440

Emerald Group Publishing Ltd

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The Direct Stress Anal/sis of Swept Cantilever Plates of Low Aspect Ratio: An Approximate Method, employing the Principle of Least Work, which Obviates the Need for Intermediate Deflection Calculations

By A.F.R.Ae.S. A. Coull   B.Sc.(Eng.)   D.C.Ae.   Ph.D.  

Aircraft Engineering, Vol. 37, Iss. 6, 1993-12 ,pp. : 182-190

Emerald Group Publishing Ltd

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Torsion of a Multi-webbed Rectangular Tube: An Exact Solution of the Problem Treated Approximately by Mr Mansfield

By A.F.R.Ae.S. W.H. Wittrick   M.A.   Ph.D.  

Aircraft Engineering, Vol. 25, Iss. 12, 1993-12 ,pp. : 372-372

Emerald Group Publishing Ltd

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The Warping and Constraint of Certain Rectangular Box Sections: Calculation of the Effect on a Simple Type of Shell of the Results of Torsion and Flexure

By B.A. M. Fine  

Aircraft Engineering, Vol. 22, Iss. 6, 1993-12 ,pp. : 172-173

Emerald Group Publishing Ltd

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