Creep Deflexion and Stress Distribution in a Beam: Analysis for a Rectangular Beam Subjected to a Constant Bending Moment

Author： A.F.R.Ae.S. W.J. Goodey   M.A.  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.30, Iss.6, 1993-12, pp. : 170-172

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

The Stress-Strain Characteristics of a Magnesium Alloy Beam: Behaviour when Electrically and Plastically Deformed by a Uniform Bending Moment at Room Temperature

By A.M.I.Mech.E. A.E. Johnson   M.Sc.   M.Sc.Tech.   B.Sc. D.C. Herbert  

Aircraft Engineering, Vol. 20, Iss. 11, 1993-12 ,pp. : 330-334

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Reduction of Bending Moment at the Root of a Rotor Blade: Effects of Replacing Elastic Beam-type Flapping Hinge by Leaf Springs

By Leeuwen H.P. van  

Aircraft Engineering, Vol. 32, Iss. 10, 1993-12 ,pp. : 309-310

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Shear Stress in a Tapering Beam

By M.Sc. G.B. Saksena  

Aircraft Engineering, Vol. 16, Iss. 2, 1993-12 ,pp. : 47-50

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Trailing Edge Flap Activated by a Piezo-Induced Bending-Torsion Coupled Beam

By Bernhard Andreas P. F.   Chopra Inderjit  

Journal of the American Helicopter Society, Vol. 44, Iss. 1, 1999-01 ,pp. : 3-15

AHS International

Access to resources Recommend Favorite

A New Piston-Ring Tester: The Amsler Type K337, which Exerts a Constant Bending Moment over the Entire Circumference

By  

Aircraft Engineering, Vol. 10, Iss. 7, 1993-12 ,pp. : 218-218

Emerald Group Publishing Ltd

Access to resources Recommend Favorite