05.10.2012 Views

Broch

Broch

Broch

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

STRUCTURAL DESIGN<br />

General<br />

Building practice approximation<br />

method<br />

for calculation of<br />

cutting forces and<br />

deformations.<br />

Version 1 / 2011<br />

M1 BSP crossplan<br />

Components made of M1 BSP crossplan are designed and executed according to the following<br />

standards:<br />

• Design according to DIN 1052:2008 allowing for German technical approval<br />

(Z-9.1-638)<br />

or<br />

• Design according to EN 1995 (Eurocode 5) allowing for Appendices 2 to 4 of European<br />

technical approval ETA-09 / 0036<br />

The structural analysis for M1 BSP crossplan must be conducted in each individual case and<br />

the standards and regulations applicable at the site of use must be complied with.<br />

Analysis of the stress distribution and internal forces and moments must be conducted according<br />

to the composite theory allowing for shear deformations.<br />

An approximation method is required in practical use. Here, the calculation is carried out as<br />

for a beam under bending moment with fl exible joining means (Austrian standard B 4100 / 2;<br />

DIN 1052; EN 1995-1-1, Appendix B), but the shear deformation of the transverse layers is<br />

taken into consideration instead of the fl exibility of the joining means.<br />

Using this approach, it is possible to achieve a good approximation for the stress and deformation<br />

calculations.<br />

At the same time, for the actual design the moments of inertia are multiplied by a reduction<br />

factor - which takes into account the net moments of inertia and the rolling shear deformation<br />

of the transverse layers.<br />

Using the eff ective moments of inertia (Ieff ) obtained as a result, it is possible to calculate<br />

the cutting forces and deformations as for beams under bending moment with a rigid bond.<br />

M Q<br />

Lamellas stressed in the direction of the fibres<br />

� High stiffness<br />

Cross-section<br />

Q<br />

Tension<br />

Lamellas stressed transverse to the direction of the fibres<br />

� No stiffness E = 0<br />

M<br />

σ = 0<br />

Normal stress due to bending<br />

Pressure<br />

σ = 0<br />

Shear stress<br />

Rolling shear transversally<br />

Rolling shear transversally<br />

Note:<br />

The solution only applies exactly for single span beams with sinusoidal uniform load. It should<br />

also be noted that the eff ective moments of inertia Ieff depend on the width between supports<br />

of the panels. The shorter the width between supports, the greater the proportion of<br />

shear deformation and thus also the percentage reduction of the moments of inertia (compare<br />

table of cross-sectional values). Beyond this, a more accurate calculation method is<br />

necessary particularly in the case of point loads and very short beam lengths.<br />

In the case of continuous beams, the width between supports of the fi eld concerned should<br />

be used for the width between supports for selection of the eff ective moment of inertia 4 / 5<br />

Ieff , in the case of cantilever beams double the protruding length should be used (cf. EN<br />

1995-1-1, Appendix B). However, calculation of the cutting force and deformation must be<br />

performed using the actual widths between supports or protruding lengths.<br />

This approximation method is also the basis of the design charts.<br />

Mayr-Melnhof Kaufmann 9

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!