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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Spar Web Buckling of a Supersonic Aircraft: An Analysis of a Simply-Supported Rectangular Plate Under the Action of In-Plane Stresses Due to the Action of Aerodynamic and Inertia Forces and Kinetic Heating Effects

By D.C.Ae. J.P.H. Webber   M.Sc. D.S. Houghton  

Aircraft Engineering, Vol. 35, Iss. 12, 1993-12 ,pp. : 364-368

Emerald Group Publishing Ltd

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One Integrable Case of the Perturbed Two-Body Problem

By Poleshchikov S. M.  

Cosmic Research, Vol. 42, Iss. 4, 2004-07 ,pp. : 398-407

MAIK Nauka/Interperiodica

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The Continuous Beam: The Case of Irregular Lateral Loading Combined with End Loads

By A.K.C. S.J.E. Moyes   B.Sc.  

Aircraft Engineering, Vol. 10, Iss. 8, 1993-12 ,pp. : 243-247

Emerald Group Publishing Ltd

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Technical Notes: The Rotor Blade Flap Bending Problem—An Analytical Test Case

By Harris Franklin D.  

Journal of the American Helicopter Society, Vol. 37, Iss. 4, 1992-10 ,pp. : 64-67

AHS International

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