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Calculation of Shear Areas and Torsional Constant using the Boundary Element Method with Scada Pro

8

called shear deformation coefficient

1

a

, while with the aid of these coefficients the

shear areas of the cross-section of the beam can be easily derived, as will occur in the next.

More specifically, the shear areas of the beam cross-section loaded by constant shear

force (

y

Q

,

z

Q

components, along y, z axis, respectively) are given by the

equations

y

y

y

A

A A

,

  

z

z

z

A

(3.1a,b)

while, the cross-section shear rigidities of the Timoshenko’s flexural beam theory are

identified as

y

y

y

GA

GA GA

,

 

z

z

z

G

G

GA

(3.2a,b)

where, the shear deformation coefficients

y

,

z

are determined by the equations [3.1-3.3]

2

2

2

2

cy

cy

y

y

AG

d

y

z

Q

 

 

 

(3.3a)

2

2

2

2

cz

cz

z

z

AG

a

d

y

z

Q

 



(3.3b)

In equations (3.3a,b) the

cy

,

cz

are the (shear) warping functions resulting from solving

the following boundary value problem [3.1-3.3]

 

2

2

2

2

2

1

,

c

c

c

z zz

y zz

yy zz

y z

Q I

z Q I y

GI I

y

z

 

   

 

in

Ω

(3.4a)

0

c

n

on

Γ

(3.4b)

for cases

0

y

Q

,

0

z

Q

and by defining

,

cy

y z

as the resulting warping function

0

y

Q

,

0

z

Q

and by defining

,

cz

y z

as the resulting warping function

In the previous, we have consider a beam with constant (along the longitudinal axis of the

beam) cross-section with an arbitrarily shaped occupying the two-dimensional simply or

multiply connected region

Ω

of the

y; z

plane bounded by the curve

Γ

. The aforementioned

boundary value problem arises from the equation of equilibrium of the three-dimensional

theory of elasticity neglecting the body forces and the physical consideration that the

traction vector in the direction of the normal vector

n

vanishes on the free surface of the bar.

The numerical solution of the boundary value problem stated above (3.4a,b) for the

evaluation of the (shear) warping functions

cy

and

cz

is accomplished employing a pure

BEM approach [3.4], that uses only boundary discretization. Finally, since the torsionless

bending problem (transverse shear loading problem) of beams is solved by the BEM, the