Objective

To determine the stress–strain state of a symmetric wedge of unit thickness subjected to bending by a uniformly distributed load.

Reference

Demidov S.P., Theory of Elasticity, Moscow, Vysshaya Shkola, 1979.

Problem statement

To determine the stress σrr in the wedge at a distance of r = 5 m from the apex for the case of wedge bending under a uniformly distributed load, as well as the angle θ0 at which σrr=0.

Design model

A uniformly distributed load of intensity q is applied to the upper face of the wedge of unit thickness.

Початкова геометрія аналітичної схеми

Початкова геометрія СЕ моделі

a

b


Initial geometry of: a - analytical model; b - FE model

Geometry

Wedge thickness h = 1 m
Radius defining the wedge domain R = 15 m
Wedge apex angle 2α = 30°

Material properties

Modulus of elasticity Е = 3 * 107 kPa
Poisson's ratio ν = 0.2

Boundary conditions

Restraints in all degrees of freedom are applied along the arc boundary of the wedge.

Loads

Uniformly distributed load: q = 10 kN/m

Output data

Розрахункова і деформована схеми

Design and deformed shapes

Мозайка напружень σrr (Ny), кН/м2 (фрагмент схеми)

Мозайка напружень σrr (Ny) з відображенням кута θ0, °

a

b


Mosaic plot of stress σrr (Ny), kN/m2: a - model fragment; b - with angle indication θ0

Analytical solution

K = tgα-α
σrr = q(2α-2θ-(1-cos2θ)*tgα)-sin2θ)/2K
σθθ = q(2α-2θ-(1+cos2θ)*tgα)+sin2θ)/2K
σ = q(1-tgα*sin2θ-cos2θ)/2K

Comparison of calculation results:

Without additional side nodes:

Point The unknown Analytical solution LIRA-FEM Error, %
r = 5 m when θ = 0 Ny, kN/m2 98 94,635 3,4337
r = 5 m when θ = α Ny, kN/m2 -107 -104,63 2,215
σrr = 0 θ0, ° 13,4 14,25 5,9649

With additional side nodes:

Point The unknown Analytical solution LIRA-FEM Error, %
r = 5 m when θ = 0 Ny, kN/m2 98 94,974 3,0878
r = 5 m when θ = α Ny, kN/m2 -107 -104,97 1,8972
σrr = 0 θ0, ° 13,4 14,25 5,9649

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