Composite I-Section Beams: Their Properties when Subjected to Bending Stresses, with Particular Reference to Steel-Duralumin Beams

By I.E.E. Leslie P. Dudley   D.F.H.   Grad.  

Aircraft Engineering, Vol. 9, Iss. 6, 1993-12 ,pp. : 165-166

Emerald Group Publishing Ltd

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Thermo-Elastic Formulae for the Analysis of Beams: Stress Distributions within a Structure due to Temperature Gradients and their Influence on Strength and Stiffness

By F.R.Ae.S. W.S. Hemp   M.A.  

Aircraft Engineering, Vol. 28, Iss. 11, 1993-12 ,pp. : 374-376

Emerald Group Publishing Ltd

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Torsion in Box Beams: Some Notes on the Effect of End Constraint in Torsion Boxes of Rectangular Section

By A.F.R.Ae.S. J.H. Payne   B.Sc.   A.C.G.I.   D.I.C.  

Aircraft Engineering, Vol. 14, Iss. 1, 1993-12 ,pp. : 2-8

Emerald Group Publishing Ltd

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Torsion of a Constrained Rectangular Box Section: An Experimental Investigation of the Stresses due to Torsion in a Rectangular Box Section with one end Constrained

By M.Sc.Tech. W.L Green   A.M.I.Mech.E. S.S. Gill   M.ScTech.   Ph.D.  

Aircraft Engineering, Vol. 26, Iss. 2, 1993-12 ,pp. : 34-35

Emerald Group Publishing Ltd

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The Analysis of Fuselages of Arbitrary Cross-section and Taper

By Argyris J.H.   Kelsey S.  

Aircraft Engineering, Vol. 31, Iss. 4, 1993-12 ,pp. : 101-112

Emerald Group Publishing Ltd

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