Table of Contents Table of Contents
Previous Page  129 / 228 Next Page
Information
Show Menu
Previous Page 129 / 228 Next Page
Page Background

4. STRUCTURAL DESIGN OF LVL STRUCTURES

4.3.9 Stability of LVL members

LVL cross sections are usually slender, as it is economical to

produce panel billets and cut thin and high or deep beams and

stud dimensions. Stability calculation is therefore particularly

important for LVL beams.

Column stability and lateral torsional stability shall be ver-

ified using the characteristic stiffness properties

E

0,05

and

G

0,05

.

4.3.9.1 Members subjected to combined bending

and axial compression or tension

Roof rafters of pitched roofs are typical members which shall

be analysed for combined bending and compression. Accord-

ing to Eurocode 5, the expressions (4.17) & (4.18) or (4.19) &

(4.20) shall be fulfilled.

For combined bending and axial tension the following ex-

pressions shall be satisfied:

σ_(t,0,d)/f_(t,0,d) +σ_(m,y,d)/(k_(m,α (4.17) (EC5 6.17)

σ_(t,0,d)/f_(t,0,d) +k_m σ_(m,y,d)

(4.18) (EC5 6.18)

For combined bending and axial compression the following

expressions shall be satisfied:

(σ_(c,0,d)/f_(c,0,d) )^2+σ_(m,y,d)/(

(4.19) (EC5 6.19)

(σ_(c,0,d)/f_(c,0,d) )^2+k_m σ_(m,

(4.20) (EC5 6.20)

where

k

m

makes allowance for re-distribution of stresses and the

effect of inhomogeneities of the material in cross-section.

For rectangular LVL cross sections

k

m

= 0,7 and for other

cross sections

k

m

= 1,0; and

k

m,α

is a factor for combined stresses in tapered beams, see

subsection 4.3.11. For straight beams

k

m,α

=1,0.

4.3.9.2 Columns subjected to either compression or

combined compression and bending

According to Eurocode 5, the expressions (4.20) & (4.21) shall

be fulfilled.

σ_(c,0,d)/〖k_(c,y)∙f〗_(c,0,d) +σ_(m (4.29) (EC5 6.23)

σ_(c,0,d)/〖k_(c,z)∙f〗_(c,0,d) +k_m∙σ

(4.30) (EC5 6.24)

When both

λrel,z

≤ 0,3 and

λrel,y

≤ 0,3 the stresses should sat-

isfy the expressions (4.19) and (4.20) of combined bending and

axial compression. In all other cases the stresses, which will

be increased due to deflection, should satisfy the expressions

(4.29) and (4.30).

k_(c,y)=1/(k_y+√(k_y^2-λ_(rel,y)^2 ))

(4.31)(EC5 6.25)

k_(c,z)=1/(k_z+√(k_z^2-λ_(rel,z)^2

(4.32) (EC5 6.26)

k_y=0,5(1+β_c (λ_(rel,y)-0,3)+λ_(rel,y)^2 (4.33) (EC5 6.27)

k_z=0,5(1+β_c (λ_(rel,z)-0,3)+λ_(rel,z)^2 (4.34) (EC5 6.28)

Factor

β

c

is 0,10 for LVL members within the straightness

limit of L/500. The limit is defined in Eurocode 5, Section 10 as

the deviation from straightness measured midway between the

supports of frame members, columns and beams where lateral

instability can occur.

The relative slenderness ratio should be taken as:

λ_(rel,y)=λ_y/π √(f_(c,0,k)/E_0,05 )

(4.35) (EC5 6.21)

λ_(rel,z)=λ_z/π √(f_(c,0,k)/E_0,05 )

(4.36) (EC5 6.22)

Where

λ

y

and

λ

rel,y

are the slenderness ratio corresponding to

bending about the y-axis (deflection in the

z-direction);

λ

z

and

λ

rel,z

are the slenderness ratio corresponding to

bending about the z-axis (deflection in the

y-direction); and

E

0,05

is the characteristic value of modulus of elasticity

parallel to the grain.

For rectangular cross section the slenderness of a member is

defined as:

λ=l_c/i=l_c/√((I/A) )=l_c/√((((bh^3)/12))/bh)=√12

(4.37)

where

l

c

is the buckling length; and

h

is the height of the member in the direction of the buckling

analysis.

The buckling coefficient kc for different LVL classes and slen-

derness ratios are shown in Figure 4.18 and Table 4.8. The val-

ues are very similar for all shown LVL classes.

More advanced instructions on determining the effect of

an angle to the grain on LVL strength properties may be found

in the manufacturers’ technical documentation.

t,0,d t,0,d

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

(4.17) (EC5 6.17)

t,0,d t,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

(4.18) (EC5 6.18)

c,0,d c,0,d

2

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

(4.19) (EC5 6.19)

c,0,d c,0,d

2

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

(4.20) (EC5 6.20)

t,0,d t,0,d

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

(4.17) (EC5 6.17)

t,0,d t,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

4.18 (EC5 6.18)

, , , ,

� +

m,y,d ,α

,y,d

+

m

, , , ,

≤ 1

19 E 19

c,0,d c,0,d

2

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

(4.20) (EC5 6.20)

t,0,d t,0,d

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

(4.17) (EC5 6.17)

t,0,d t,0,d

+

m

m,y,d m,α

m,y,

+

m,z,d m,z,

≤ 1

(4.18) (EC5 6.18)

c,0,d c,0,d

2

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

(4.19) (EC5 6.19)

c,0,d c,0,d

2

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

(4.20) (EC5 6.20)

t,0,d t,0,d

+

m,y,d m,α

m,y,d

+

m

,z, m,z,d

≤ 1

(4.17) (EC5 6.17)

t,0, t,0,d

+

m

m,y,d m,α

m,y,d

+

,z,d m,z,d

≤ 1

(4.18) (EC5 6.18)

c,0,d c,0,d

2

+

m,y,d m,α

m,y,d

+

m

,z, m,z,d

≤ 1

(4.19) (EC5 6.19)

c,0,d c,0,d

2

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

(4.20) (EC5 6.20)

c,0,d c,y

c,0,d

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

(4.29) (EC5 6.23)

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

(4.30) (EC5 6.24)

c,y

=

1

y

+�

y2

rel,y 2

(4.31) (EC5 6.25)

1

(4.32) (EC5 6.26)

c,0,d c,y

c,0,d

+

m,y,d m,α

m,y,d

+

m

, , m,z,d

≤ 1

(4.29) (EC5 6.23)

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

, , m,z,d

≤ 1

(4.30) (EC5 6.24)

c,y

=

1

y

+�

y2

rel,y 2

(4.31) (EC5 6.25)

(4.32) (EC5 6.26)

c,0,d c,y

c,0,d

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

c,y

=

1

y

+�

y2

rel,y 2

c,z

=

1

z

+�

z2

rel,z 2

y

= 0,5�1 +

c

rel,y

− 0,3� +

rel,y 2

z

0,5�1 +

c

rel,z

− , �

rel,z 2

rel,y

=

y

c,0,k 0,05

rel,z

=

z

c,0,k 0,05

=

c

=

c

�� �

=

c

� ℎ 3 12 � ℎ

= √12 �

c

c,0,d c,y

c,0,d

+

,y,d ,α

,y,d

+ ∙

m,z,d m,z,d

≤ 1

c,0,d c,z

c,0,d

,y,d ,α

,y,d

,z,d m,z,d

c,y

1

y y2 rel,y 2

c,z

1

z

z2 rel,z 2

y

, �1

c

rel,y

, �

rel,y 2

z

= 0,5�1 +

c

rel,z

− 0,3� +

rel,z 2

rel,y

y c,0,k 0,05

rel,z

=

z

c,0,k 0,05

c

c

� �

c � ℎ 3 12 � ℎ

c

c,0,d c,y

c,0,d

+

m,y,d m,α

m,y,d

+

m

m,z,d m,z,d

≤ 1

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

c,y

=

1

y

+�

y2

rel,y 2

c,z

=

1

z

+�

z2

rel,z 2

y

= 0,5�1 +

c

rel,y

− 0,3� +

rel,y 2

z

= 0,5�1 +

c

rel,z

− 0,3� +

rel,z 2

rel,y

=

y

c,0,k 0,05

rel,z

=

z

c,0,k 0,05

=

c

=

c

�� �

=

c

� ℎ 3 12 � ℎ

= √12 �

c

c,0,d c,y

c,0,d

+

m,y,d m,α

m,y,d

+

m

,z,d ,z,

≤ 1

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

c,y

=

1

y

+�

y2

rel,y 2

c,z

=

1

z

+�

z2

rel,z 2

y

,

c rel,y

,

rel,y 2

z

= 0,5�1 +

c

rel,z

− 0,3� +

rel,z 2

rel,y

=

y

c,0,k 0,05

rel,z

=

z

c,0,k 0,05

=

c

=

c

�� �

=

c

� ℎ 3 12 � ℎ

= √12 �

c

c,0,d c,y

c,0,d

+

m,y,d m,α m,y,d

+

m

m,z,d m,z,d

1

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

,y

y y rel,y

c,z

=

1

z

+�

z2

rel,z 2

y

= 0,5�1 +

c

rel,y

− 0,3� +

rel,y 2

z

= 0,5�1 +

c

rel,z

− 0,3� +

rel,z 2

rel,y

y c,0,k 0,05

rel,z

=

z

c,0,k 0,05

=

c

=

c

�� �

=

c

� ℎ 3 12 � ℎ

= √12 �

c

c,0,d c,y

c,0,d

m,y,d m,α

m,y,d

m

m,z,d

1

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d m,z,d m,z,d

≤ 1

c,y

1

y y2 rel,y 2

c,z

1

z

+�

z2

rel,z 2

y

0,5�1

c

rel,y

0,3�

rel,y 2

z

0,5�1

c

rel,z

0,3�

rel,z 2

l,y

y c,0,k 0

rel,z

=

z

c,0,k 0,05

=

c

=

c

�� �

c

� ℎ 3 12 � ℎ

√12 �

c

c,0,d c,y

, ,

+

m,y,d m,α

m,y,d

+

m

, , , ,

c,0,d c,z

c,0,d

+

m

m,y,d m,α

m,y,d

+

m,z,d m,z,d

≤ 1

c,y

1

y

+�

y2

rel,y 2

c,z

=

1

z

+�

z2

rel,z 2

y

= 0,5�1 +

c

rel,y

− 0,3� +

rel,y 2

z

= 0,5�1 +

c

rel,z

− 0,3� +

rel,z 2

y

y

c,0,k ,

rel,z

=

z

c,0,k 0,05

=

c

=

c

�� �

=

c

� ℎ 3 12 � ℎ

= √12 �

c

LVL Handbook Europe

127