# Plate Buckling ABS 2004

An important aspect in the design of an offshore steel structure is the buckling and ultimate strength behavior of its fundamental structural components. To ensure high technical quality plate buckling check according to ABS 2004 Guide for Buckling and Ultimate Strength assessment for offshore structures, APRIL 2004 (updated February 2012)

Guide for Buckling and Ultimate Strength Assessment for offshore structures

All used formulas from the standard are below calculation in approach chapter.

### Calculation approach

For individual loads and loads sets plate buckling is calculating based on formulas using stresses from load. For Load Group plate buckling is calculated as envelop. Load Group items are calculated using formulas and then min/max/abs is found. Load Group contains the worst values for each parameter and gives a possibility to check the highest Ultimate Strength and Buckling State Limits for all items at once.

Ultimate Strength Limit and Buckling State Limit depend on plate results (stresses) and plate dimensions (length, width and thickness).

Plate buckling check includes various options for stresses to be checked:

- Element Stress: MidPlane (no bending) or Average;

- Use Plate Average Stress - stress is averaged on plate using elements area. Calculation is performed on every element but with averaged plate stresses.

- Use Absolute Shear for plate average (Conservative);

Note: for x and y direction only compression (negative) stresses is used in calculations. Positive stress is ignored and set 0. For the shear (xy) direction positive and negative stresses are used.

__Stress Conversion.__ Plate buckling check require to verify stresses into plate direction (direction of longest plate edge). Element Sx stress will be translated into plate length direction, element Sy into width direction.

Conversion of stresses is done automatically in plate buckling check. For average option first stresses are averaged and afterwards translated. For MinMidplane option midplane stresses are translated and then minimum values are taken.

It is possible to turn off automatically conversion of stresses to plate direction (Convert Stress to Plate Direction option). Only in case when stresses are oriented correctly by Femap analysis (by Material direction) and correct plate direction can't be recognized (stiffener are not modeler yet or mesh not coincide) set option to OFF. Please contact support if extra explanation is required: support@sdcverifier.com

SDC Verifier makes an assumption that plate elements are calculated without any output transformation and default values are used:

- For triangle elements x stress is oriented along first ege (node1 -> node2 define 1 edge).
- For quad elements x stress is oriented along Diagonal Bisector:

Execute in Femap main menu:

- - and press . Check if orientation set to default values.__Dimensions.__ Results depend on plate dimensions and direction and it is important to understand how Panel Finder perform recognition. Length is considered the longest edge of plate and width the longest perpendicular to longest edge:

__Plate Thickness.__ Calculations are performed on every element and thickness is taken directly from each element. It is possible to set thickness manually, in this case element thickness will be ignored and user defined thickness will be used.

Example: Plate with 2 properties 0.01 and 0.02 thicknesses. Left picture display property labels with property thicknesses and right presents plate buckling plot of thickness parameter:

#### Buckling State Limit

The buckling state limit for plate panels between stiffeners is defined by the following equation:

Where

η - maximum allowable strength utilization factor.(1 / Safety Factor, e.g. Sf = 1.25 then η = 1 / 1.25 = 0.8).

σ_{xmax}/σ_{ymax} - maximum compressive stress in the longitudinal / transverse direction

- edge shear stress

- critical buckling stress for uniaxial compression in the longitudinal / transverse direction.

- critical buckling stress for edge shear.

P_{r} = 0.6 for steel, proportional linear elastic limit of the structures.

σ_{o} = F_{y} - Yield Stress.

*t* - plate (element) thickness, *s* - plate width, *v* - poison ratio = 0.3.

Buckling coefficient k_{s} is calculated:

k_{s} = 4.0*C_{1} - for longitudinal direction;

- for transverse direction

- for shear direction.

Where *s* / *l* - plate width to length ratio.

The coefficient C_{1} is equal to:

- 1.1 for plate panels between angles or tee stiffeners;
- 1.0 for plate panels between flat bars or bulb plates;
- 1.0 for plate elements, web plate of stiffeners and local plate of corrugated panels.

C_{2} can be defined:

- 1.2 for plate panels between angles or tee stiffeners;
- 1.1 for plate panels between flat bars or bulb plates;
- 1.0 for plate elements and web plates.

#### Ultimate Strength

The ultimate strength limit for plate panels between stiffeners is defined by the following equations:

η - maximum allowable strength utilization factor. (1 / Safety Factor, e.g. Sf = 1.25 then η = 1 / 1.25 = 0.8).

- ultimate strength with respect to uniaxial stress in the longitudinal direction (not less than critical x buckling stress).

- ultimate strength with respect to uniaxial stress in the transverse direction (not less than critical y buckling stress).

- ultimate strength with respect to edge shear (not less than critical shear buckling stress).

- plate length to width ratio.

- Yield Stress.

- coefficient to reflect interaction between longitudinal and transverse stresses. (negative values are acceptable).

- slenderness ratio.

### Adding ABS 2014 in SDC Verifier:

To add ABS 2004 standard execute

- from main menu. Alternatively use context menu:- critical buckling stresses is multiplied on utilization factor.

- increases each plate thickness (e.g. 1.1 increase on 10%) and decreases stresses;

- is proportional linear elastic limit of the structures, which may be taken as 0.6 for steel;

Calculations are performed for each element with converted stresses (into plate direction) or Plate Average Stresses and using Plate dimensions.

- what stress to check.

- average stress among element point of interests.

- minimum midplane stress (Stop + Sbottom / 2), without bending.

- used only together with plate average option and means that absolute shear is used for plate averaging:

With Absolute Shear option higher shear stress is used for checking, that makes verification more conservative.

Convert Stress into Plate Direction option allows to turn off automatic stress translation into plate direction. Almost in all cases it should be ON, see calculation approach for explanation when to turn off this option.

Formulas of Plate Buckling ABS standard use Yield Stress from materials. It is important to set this value for each material. Standard check if all Yield Stress is not equal to zero:

If count > 0 then press to edit Yield Stress:

Plate Buckling Check is calculated on Sections. With help of Panel Finder tool it is possible to automatically recognize Section and Plates with their dimensions.

By default All Sections included into selection but can be changed by pressing . If sections was not recognized press to run Panel Finder tool.

Check is passed if Ultimate Strength Limit <= 1 and Buckling State Limit <= 1.

#### Criteria Plot

Select Load, Parameter, Values to plot, View and Sections to Plot.

Parameter is set by default to last one - Buckling State Limit.

should be selected using- can use for plotting: element values, min plate, max plate and average plate (last 3 variants use one value for full plate).

- defines location of model and display options. It can be selected from the list of existing, created new one or modified.

- gives is a possibility to filter elements/node selection based on result criteria (type): Below, Above, Between, Outside. If option is set, the absolute result value is compared to selected criteria.

#### Expand / Extreme Tables

Expand Table display results for each selected section and its plates.

Extreme table show only min/max and absolute maximum results among selected sections.

should be selected usingDefine sections to be displayed in table by pressing .

- results of plate buckling are displayed over plates. This option helps to display results for each plate taking the worst result from all elements of the plate.

If **Min, Max, Absolute max** is selected - the worst result is taken from all parameters of the check;

If **Related to Last Parameter is** selected - the worst result will be taken only from last parameter of the check. The rest results for plate will be taken only from that one element which contains the worst result by selected Search Type. Available for expand table only.

- displays results over plates for each section if turned on. Otherwise displays results over sections only. Available for expand table only.

#### Expand flow table

An Expand flow table displays results of the selected section and its plates for multiple loads.

Loads should be selected using Multiple Load Selector;

Select section to be used by pressing . Window with the list of available sections will be displayed:

- the results of plate buckling are displayed over the plates. This option helps to display the results for each plate taking the worst result from all elements of the plate.

- the worst result is taken from all parameters of the check;

- the worst result will be taken only from the last parameter of the check. The rest results for plate will be taken only from that one element which contains the worst result by the selected Search Type.

- displays results over the plates for each load if turned on.