Use of chromoplastic models for the study of the behaviour of rectangular plates after buckling

By Eng NICOLAE D. POPESCU-CASTELLIN   Dr  

Aircraft Engineering, Vol. 45, Iss. 1, 1993-12 ,pp. : 4-7

Emerald Group Publishing Ltd

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The Buckling of Tapered Plates in Compression: Compressive Buckling under Varying Loading of Simply Supported Plates Simultaneously Tapered in Plan Form and in Thickness

By Klein Bertram  

Aircraft Engineering, Vol. 28, Iss. 12, 1993-12 ,pp. : 427-430

Emerald Group Publishing Ltd

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Double Block Shear Test for Foil Honeycomb Cores: Re-examination of This Method as Means of Measuring the Shear Modulus

By D.C.Ae. H.P. O'Sullivan  

Aircraft Engineering, Vol. 33, Iss. 3, 1993-12 ,pp. : 64-66

Emerald Group Publishing Ltd

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Shear Stresses in Hollow Sections: An Account of the Theory of Stresses in Bending and Torsion for Designers of Stressed-Skin Structures

By M.A. W.J. Goodey  

Aircraft Engineering, Vol. 8, Iss. 4, 1993-12 ,pp. : 93-102

Emerald Group Publishing Ltd

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The Bending Stresses in Cantilever Plates by Moiré Fringes: An Experimental Technique giving Directly the Gradient at all Points on a Model's Surface

By A.Inst.P. P.J. Palmer   Ph.D.   M.Sc.   D.I.C.   A.R.C.S.   A.F.R.Ae.S.  

Aircraft Engineering, Vol. 29, Iss. 12, 1993-12 ,pp. : 377-380

Emerald Group Publishing Ltd

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