Buckling
The second order effects are taken into account for the members loaded by compressive force in accordance with the chapter 5.8 of EN 1992-1-1. Following methods are avalable:
- Method based on the nominal stiffness
- Method based on the nominal curvature
- Simplified method based on 12.6.5.2 of the standard (only plain concrete)
Slenderness criterion
The detailed analysis is performed if the slenderness is greater than limiting value λlim. The limiting slenderness is given by the expression 5.13N:
Where is: | λlim |
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A, B, C |
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n |
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The coefficient A is given by the expression:
Where is: | φef |
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The coefficient B is given by the expression:
Where is: | ω |
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The mechanical reinforcement ratio ω is given by the expression:
Where is: | As |
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fyd |
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Ac |
| |
fcd |
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The coefficient C is given by the expression:
Where is: | rm |
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The moment ratio rm is given by the expression:
Where is: | M01, M02 |
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The relative normal force n is given by the expression:
Where is: | NEd |
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Ac |
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fcd |
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Method based on the nominal stiffness
This method is based on the chapter 5.8.7. The nominal stiffness is given by expression (5.21):
Where is: | Kc |
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Ecd |
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Ic |
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Ks |
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Es |
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Is |
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The factor Kc is given by expression (5.22):
Where is: | k1 |
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k2 |
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φef |
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The factor k1 is given by expression (5.23):
Where is: | fck |
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The factor k2 is given by expression (5.24):
Where is: | n |
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λ |
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The buckling load based on the nominal stiffness is calculated using expression:
Where is: | NB |
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EI |
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l0 |
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The total design moment, including second order moment, is calculated using formula (5.28):
Where is: | M0Ed |
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β |
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NB |
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NEd |
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The factor β is given by expression (5.29):
Where is: | c0 |
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The value of the factor c0 is the input in the software. Following values are recommended according to the chapter 5.8.7.3(3):
Factor c0 | The distribution of first order moment |
8.0 | constant |
9.6 | parabolic |
12 | symmetric triangular |
Method based on the nominal curvature
This method uses procedures given in the chapter 5.8.8. The nominal curvature is given by the expression (5.34):
Where is: | 1/r |
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Kr |
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Kφ |
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The curvature 1/r0 is given by following formula:
Where is: | ε0 |
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d |
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The strain of reinforcement at yield strength ε0 is calculated using this formula:
Where is: | fyd |
|
Es |
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The effective depth of a cross-section is given by the expression (5.35):
Where is: | h |
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is |
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The factor Kr is given by the expression (5.36):
Where is: | n |
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nbal |
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The relative axial force nu is calculated using the formula:
Where is: | ω |
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The factor Kφ is given by the expression (5.37):
Where is: | β |
|
φef |
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The factor β is given by the expression:
Where is: | fck |
|
λ |
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The nominal second order moment M2 is given by the expression (5.33):
Where is: | NEd |
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e2 |
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he deflection e2 is calculated using formula
Where is: | 1/r |
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l0 |
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c |
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The value of the factor c is the input in the software. Following values are recommended according to the chapter 5.8.8.2(4):
Factor c | Curvature distribution |
8.0 | constant |
10 | sinusoidal |
The design moment is given by the expression (5.31):
Where is: | MEd |
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M0Ed |
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M2 |
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Simplified design method according to 12.6.5.2
This method may be used for plain concrete and lightly reinforced members according to the chapter 12.6.5.2 of EN 1992-1-1. The design axial resistance is given by the expression (12.10):
Where is: | b |
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hw |
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fcd |
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Φ |
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The factor Φ is given by the expression (12.11):
The eccentricity etot is calculated using following formula:
Where is: | e0 |
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ei |
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l0 |
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