Deflexion of Tapered Beams: The Case of Cantilever Beams with Lateral and End Loads

By B.A. R. Tatham   Ph.D. H.L. Price  

Aircraft Engineering, Vol. 17, Iss. 11, 1993-12 ,pp. : 312-329

Emerald Group Publishing Ltd

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Tapered Geometries for Improved Crashworthiness Under Side Loads

By Fleming David C.   Vizzini Anthony J.  

Journal of the American Helicopter Society, Vol. 38, Iss. 1, 1993-01 ,pp. : 38-44

AHS International

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Tapered Beams: Suggested Solutions for Some Typical Aircraft Cases

By B.Sc. E.H. Atkin  

Aircraft Engineering, Vol. 10, Iss. 11, 1993-12 ,pp. : 347-351

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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Damage Analysis of Composite Tapered Beams

By Vizzini Anthony J.   Lee Sung W.  

Journal of the American Helicopter Society, Vol. 40, Iss. 2, 1995-04 ,pp. : 43-49

AHS International

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