Custom Standard

Standard is a set of checks and items to perform calculations according to formulas and rules.

To add Custom Standard execute Standards - Main - Custom from the ribbon.

Standard contains:

• Constants;
• Types;
• Characteristics;
• Classification;
• Standard Tables;
• Checks;
• Variables.

It is possible to convert a predefined (built-in) standard into Custom. Select standard and execute Convert to Custom from the Standard context menu:

Apply Values to Identical Standard - copy all the Input (Constants, Characteristics, Classifications, Standard Tables) of the standard from selected standard to another standard of the same type. Command is available only for predefined standards.

Note: command can be executed on individual item of the Input part of the standard or on a group of items (e.g. Characteristics).

Constants

Constants is a static value which can be used in checks with the help of Alias. It is useful to create constants and use them in formulas because in case of modifications (related to constants) it is required to make a change in one place only.

Constant dialog box:

Types

Standard type is a list of titles that can be used in classification or characteristic instead of numbers. To add a new type press Add from the menu:

The following dialog window will be displayed:

- add a new item;

- paste titles/aliases from the clipboard. Spaces in alias will be removed automatically;

- edit the selected item;

- remove selected items;

Import from another standard - import already existing classification type from existing standards:

Select standard, standard type and press OK to create new standard type.

Copy to standard - export all types to the existing custom standards. If type already exists it will be skipped:

 

Characteristics

SDC Verifier allows adding extra properties called Characteristics to use them in Standard check formulas. There are four types of characteristics: Material, Property, Elemental and Load.

To add Characteristics use the Characteristics context menu:

All characteristic types can be created by additional subtypes that are taken from the Types list. Numeric type is a default type and allows to apply numeric values in characteristic.

Add Material/Property Characteristic:

Set Alias to use characteristic in check formulas.

To plot characteristic values for all materials/properties press .

Add Element characteristic:

- add Node/Element group and set the value:

- edit group elements and value;

- copy selected groups with values;

- remove selected groups;

- highlight selected group nodes/elements on the model;

- plot characteristic values of selected groups;

- colored plot with selection title label of selected groups;

- colored plot with value label of selected groups;

- move selected conditions up;

- move selected conditions down.

Note: Import is available for element type characteristic only with Numeric Type.

Press Import to import Beam Length/Effective Length Factor from Beam Member Finder, Plate Width/Length and Stiffener Length from Panel Finder or Welds from Weld Finder.

All previous data from characteristic can be removed:

Import dialog box:

If Beam Member data is selected then it is required to select the direction from the list:

Note: For weld finders, only the groups with 0 values will be created.

Classification

Classification is an extra element characteristic that can be set over directions.

To add classification select type in classification Add menu item:

Numeric classification - allows to set numeric values of the classification. It is flexible as it can be used in the creation of any kind of own calculations. It is available for all types of standards. Extra classifications are possible to be created using Types. Different standards have their own predefined classifications. For example, DIN 15018 Standard predefined classifications are Element group, Weld Type and Material Type.

Set classification Alias to use it in Custom check formulas.

- add classification condition;

- edit selected condition;

- copy selected conditions;

- remove selected conditions;

- move selected conditions up;

- move selected conditions down.

Note: The first condition cannot be modified, moved, copied or removed.

- highlight selected condition elements;

- select direction to plot classification values as criteria plot or as label plot;

Selection - part of the model for which plot will be displayed;

Label Plot

Criteria Plot

Note: Values are calculated condition by condition. If the same element is a part of different conditions - the last condition value is taken. If the element does not belong to any condition - the value from the fist condition is taken.

- select welds from Weld Finder and add a list of conditions with empty classification (one weld one condition).

- classification stores values in the memory. Clear values from the memory to refresh the classification. Results of checks where classification is used wil be cleared after pressing OK button.

Classification Condition

Classification condition is applied to the selected directions of the selected elements.

Define Selection to be used in the condition.

One condition - set the value to the selected directions;

Multiple conditions - select the value for each direction separately. The directions with the same values will be grouped in one condition. Other values will form different conditions.

Use All, None, X/Y/XY buttons to operate with selected directions.

Standard Tables

Standard Table is a two-dimensional matrix of static values.

To add Standard Table press Add in Standard Tables context menu:

The following window for parameters setting will be displayed:

Set table Alias to use it in Custom check formulas.

Set count of rows and columns and press Apply to build the table.

Paste full table – paste full table from the clipboard.

Paste cell values – paste values from clipboard to cells starting from top left selected cell.

Note: To cut the table set less value for a row or a column count.

It is possible to define a row and a column Headers based on the Types List

- display chart of the selected in the following window rows/columns of data to be used for X and Y axes of the chart:

Sort X Axis Values - reorder data selected in rows in ascending order;

Alias

Alias is a unique name for Standard items through which they can be accessed in Custom check formulas.

Note: Alias can contain only letters, digits and underscore symbol ("_"). Alias is unique inside the standard and must be different from the model and result variables such as (Area, Yield, S, Abs, etc.).

Note: Alias of the standard is unique between the standards and must be different from the model and result variables.

Checks

• Custom Check;
• Custom Plate Buckling Check;
• Custom Weld Check;
• Custom Connection Check;
• Custom Rainflow Summation Check;

Common Commands

To edit parameter press . The dialog box will appear where it is possible to select the necessary parameter to edit.

To remove parameters press . The dialog box will appear where it is possible to select the necessary parameters to remove.

Press to edit multiple parameters (parameters/replacement, category and limits).

Limits are used to highlight parameters if it exceeds the limit value.

Category defines how parameter will be represented in the table (Number Format) and what Legend Settings will be applied.

E.g. Utilization Factor by default has a general format with 2 digits after the dot:

Press to move parameters:

Custom Check

Custom Check is used in SDC Verifier to perform any user-defined calculations. Custom Check consists of Parameters - formulas are made up of model variables, constants and mathematical operations, results and functions.

There are 4 predefined checks: Static Stress Check, Plate Average Stress, Plate Principal Stresses and Solid Principal Stresses.

To add Custom Check execute Add - Custom Check in the checks context menu:

Common commands are described in Common Chapter

Alias - variable name to access it from other checks.

Calculate Results over Directions - calculate for X, Y, Z, XY, YZ, ZX, Equivalent, Overall directions, otherwise one direction is calculated.

Calculate Results over Points - calculate for all element's points of interest, otherwise, one point is calculated.

Note: Calculate Results over Directions and Calculate Results over Points should be defined before the first parameter is selected.

Define Selection (by default all entities) using Selector Control to select entities that will be calculated.

Note: Only part of a model can be selected to reduce the calculation time and quickly obtain results for critical places of the model.

Load calculation can be calculated on All Loads or on Load Groups only.

If All Loads option is used then Load Group is calculated as envelope (like in Job), formulas are calculated for Individual Loads, Load Sets but Load Group is min/max/abs among its items.

If Load Groups option is used then formulas are based on group results, e.g. min/max/abs can be used for stresses, strains, line element force and plane element force.

Note: If Custom Check (no load) is created - Load Calculation Type is disabled.

Add Parameter

To add Parameter to the Custom Check press .  For each parameter, the Title and Alias must be defined.

Replacement - means the outcome is intermediate and not stored. The purpose of the replacement is to be used in other parameters from the current check and don't consume memory.

It is possible to create separate formulas for each direction. One formula will be used for all directions if it is inputted into the All Directions text field.

If the formula of a parameter contains logic operations, then the result will be 1 if the condition is fulfilled, else 0 will be assigned to the parameter value.

Note: Formulas in SDC Verifier are case insensitive.

Entities in the Main Functions contains the most important functions containing sqrt(), max(),power(), average(), etc.

All available variables of formulas are collected in the Items

- Mathematical Operations;

- Material Variables (contains characteristics, namely Young modulus, Poisson ratio, mass density, shear modulus, yield limit and tensile strength);

- Property Variables (contains the characteristics of model properties such as an area for beam type element, thickness for plate element, cross-section dimensions, etc.);

- Results Variables (Stress, Strain etc.);

- Constants from Standard;

- Characteristics;

- Classifications;

- Standard Tables;

- Inner Constants (Property Shapes, Yes, No, etc.);

- Local Check (contains Parameters already defined in the current Check);

- Check Parameter. Results from other checks from all existing standards;.

- Other variables (beam member, shape, load safety factor).

Adding Items

To add a necessary item (all except Results Variables and Check Parameters) press the corresponding button on the Items dialog box. The dialog window appears:

To Add Check Parameter press . The dialog window will be shown:

Only standards with ID ≤ current standard ID will be displayed in the list.

Checks are filtered according to the selected check type (e.g. Plate Buckling check can use results only from other Plate Buckling check.) or Load Calculation type (e.g. Custom check cannot use results from Fatigue Summation check).

All Direction/Point of Interest is available if the current check is calculated over directions/points. Otherwise, respective direction/point of interest from the source check should be selected.

To Add Result press . The dialog window will appear:

All Direction/Point of Interest is available if the current check is calculated over directions/points. Otherwise, respective direction/point of interest from the selected result should be selected.

Parameters can be edited/copied/removed or converted to characteristic using the popup menu:

Convert to characteristic - create the characteristic of the selected type where the result of parameter will be taken from the characteristic (if characteristic value ≠ 12345678), or will be calculated using the current formula:

Warning:

If the formula contains items that do not exist for certain element types (e.g. shape height does not exist for shells) then the formula will be evaluated with such items replaced with zero.

Custom check (no load).

Custom check (no load) is a sub-type of Custom Check. Check supports variables that are not based on loads (young modulus, yield stress, property area, a moment of inertia, classification, characteristics, standard table, constants etc.).

Calculate Results over Directions - optional;

Calculate Results over Points - disabled;

Load Calculation - disabled;

Selection - optional;

Property check

Property check is a sub-type of Custom Check. Check supports variables of materials, properties, constants, standard tables. Results are calculated over properties.

Calculate Results over Directions - disabled;

Calculate Results over Points - disabled;

Load Calculation - disabled;

Selection - disabled;

Plate/Stiffener Buckling

The Plate/Stiffener Buckling is used to perform plate buckling calculations with user-defined formulas.

It is very similar to the Custom Check. The major difference is that it is calculated on the section and results presented for the Sections and Plates/Stiffeners. Parameters of plate/stiffener buckling are calculating only for one direction and can use additional variables in formulas: Element Stress (Minimum compression or average) converted into plate direction and Plate dimensions.

To create Plate Buckling check execute Add - Plate/Stiffener Buckling in the checks context menu:

Plate Buckling:

Common commands are described in Common Chapter

By default, all sections are selected to be checked. Press to change Selection.

To add Parameter press . For each parameter, the Title and Alias must be defined.

Replacement - means the outcome is intermediate and not stored. The purpose of replacement is to be used in other parameters for the current check but the result is not important for the user.

Adding Items

Entities in the Main Functions contains the most important functions containing sqrt(), max(),power(), average(), etc.

All available variables of formulas are collected in the Items

- Mathematical Operations;

- Material Variables (contains characteristics, namely Young modulus, Poisson ratio, mass density, shear modulus, yield limit and tensile strength);

- Property Variables (contains the characteristics of the model properties, such as an area for beam type element, thickness for plate element, cross-section dimensions, etc.);

- Results from plates;

Results from stiffeners;

- Constants from Standard;

- Standard Tables;

- Characteristics;

- Inner Constants (Property Shapes, Yes, No, etc.);

- Local Check (contains Parameters already defined in the current Plate/Stiffener Buckling Check);

- Recognition data.

Plates:

Stiffeners:

- Check Parameter. Results from other checks from all existing standards;

Weld Check

The Weld Check is used to perform weld strength calculations with user-defined formulas.

It is very similar to the Custom Check. The major difference is that it is calculated on the welds. Parameters of weld checks are calculating only for one point of interest and 4 directions (X, Y, XY, Equivalent) and can use additional variables in formulas: Weld Force Summation in weld coordinate system.

To create Weld Check execute Add - Weld Check in the checks context menu:

Common commands are described in Common Chapter

By default, all welds are selected to be checked. Press to change Selection.

To add Parameter press . For each parameter, the Title and Alias must be defined.

Replacement - means the outcome is intermediate and not stored. The purpose of replacement is to be used in other parameters for the current check but the result is not important for the user.

Adding Items

Entities in the Main Functions contains the most important functions containing sqrt(), max(),power(), average(), etc.

All available variables of formulas are collected in the Items

- Mathematical Operations;

- Material Variables (contains characteristics, namely Young modulus, Poisson ratio, mass density, shear modulus, yield limit and tensile strength);

- Property Variables (contains the characteristics of the model properties, such as an area for beam type element, thickness for plate element, cross-section dimensions, etc.);

- Results from Weld Force Summation Tool;

- Constants from Standard;

- Standard Tables;

- Characteristics;

- Inner Constants (Property Shapes, Yes, No, etc.);

- Local Check (contains Parameters already defined in the current Weld Check);

- Recognition data.

- Check Parameter. Results from other checks from all existing standards;

Custom Connection Check

The Connection Check is used to perform calculations of the connections with user-defined formulas.

It is very similar to the Custom Check. The major difference is that it is calculated on the connections. Parameters of connection checks are calculating only for one point of interest and one direction (All) and can use additional variables in formulas: Braces Stress and Brace Classification.

To create Connection Check execute Add - Connection Check in the checks context menu:

Common commands are described in Common Chapter

By default, all connections are selected to be checked. Press to change Selection.

To add Parameter press . For each parameter, the Title and Alias must be defined.

Replacement - means the outcome is intermediate and not stored. The purpose of replacement is to be used in other parameters for the current check but the result is not important for the user.

Adding Items

Entities in the Main Functions contains the most important functions containing sqrt(), max(),power(), average(), etc.

All available variables of formulas are collected in the Items

- Mathematical Operations;

- Material Variables (contains characteristics, namely Young modulus, Poisson ratio, mass density, shear modulus, yield limit and tensile strength);

- Property Variables (contains the characteristics of the model properties, such as an area for beam type element, thickness for plate element, cross-section dimensions, etc.);

- Results from Braces Stress and Brace Classification Tools;

- Constants from Standard;

- Standard Tables;

- Characteristics;

- Inner Constants (Property Shapes, Yes, No, etc.);

- Local Check (contains Parameters already defined in the current Connection Check);

- Recognition data.

- Check Parameter. Results from other checks from all existing standards;

Custom Rainflow Summation Check

The Rainflow Summation Check is used to perform calculations on each direction and point of interest of the element and is based on the Rainflow Counting Tool data with user-defined formulas.

To create Rainflow Summation Check execute Add - Rainflow Summation in the checks context menu:

Common commands are described in Common Chapter

Category - category of result from which the Rainflow Counting data will be used;

Method - method from which the Rainflow Counting data will be used;

Selection - part of the model for which the check will be calculated;

Note: Calculations are performed only on Fatigue Groups that contain Load Groups. Therefore, results in tabes/plots can be presented only for these types of loads, depending on selected parameter.

There are 4 types of parameters:

• Rainflow Parameter - performs calculations using the data from Rainflow Counting Tool that depends on Category and Method. Not displayed in the tables/plots;
• Rainflow Summation Parameter - summarizes result for selected Rainflow Parameter and represents result of a Load Group;
• Load Group Parameter - represents result of a Load Group using one or several Rainflow Summation parameters;
• Group Summation Parameter - summarizes result of all Load Groups for selected Rainflow Summation or Load Group parameter and represents result of a Fatigue Group;
• Fatigue Group Parameter - represents result of a Fatigue Group using one or several Group Summation parameters;

For each parameter, the Title and Alias must be defined.

Rainflow Parameter

Performs calculations using the ranges calculated by Rainflow Counting Tool. Result depends on the selected Category and Method in the check. Calculations are performed for each range separately and for each point of interest of the element. Parameter can use Rainflow Counting Variables.

Note: Parameter is calculated only internally and result for it is not stored to result files. Therefore, it is not possible to select it in tables/plots to display the result.

Note: Formulas for Equivalent and Overall directions are not available to be set.

Rainflow Summation Parameter

Parameter is used to summarize result from each of the calculated range for selected Rainflow Parameter and represents result of a Load Group.

Reference Parameter - Rainflow Parameter from which the results of all calculated ranges will be summarized;

Note: Equivalent and Overall direction can use Functions and summarized results of the calculated directions of current parameter (me.x, me.y etc.).

Rainflow Load Group Parameter

Represents result of a Load Group using one or several Rainflow Summation parameters.

Rainflow Group Summation Parameter

Parameter is used to summarize result of all Load Groups for selected Rainflow Summation Parameter and represents result of a Fatigue Group.

Reference Parameter - Rainflow Summation Parameter for which the results will be calculated for each Load Group defined in Fatigue Group and will be summarized;

Use Cycles in Calculations - optionally use a proportion of the number of cycles defined in Fatigue Group of currently calculated Load Group to the summed number of cycles of all Load Groups in the Fatigue Group. In the formula the following multiplier will be added/removed: ItemNumberOfCycles / TotalNumberOfCycles which represents a portion of the result of the current Load Group comparing to other Load Groups;

Note: Equivalent and Overall direction can use Functions and summarized results of the calculated directions of current parameter (me.x, me.y etc.).

Rainflow Fatigue Group Parameter

Parameter represents result of a Fatigue Group using one or several Group Summation parameters.

Available Variables:

• Functions;
• Material Variables;
• Property Variables;
• Result Variables;
• Line Element Results Variables;
• Plate / Shell Element Results Variables;
• Plate Buckling Results Variables;
• Plate Dimensions Variables;
• Weld Results Results Variables;
• Weld Dimensions Variables;
• Stiffener Results Variables;
• Stiffener Dimensions Variables;
• Connection Results Variables;
• Connection Dimensions Variables;
• Beam Member Results Variables;
• Beam Member Dimensions Variables;
• Rainflow Counting Variables;
• Other Variables;

Functions

Variable	Value
sqrt()	Returns the square root of a specified number.
pow(,)	Returns a specified number raised to the specified power. E.g. Pow(10,2)=100
root(,)	Returns root of specified number of specified power. E.g. root(-1000, 3)=-10
min(,)	Returns smaller among specified numbers.
max (,)	Returns bigger among specified numbers.
absmax(,)	Returns the absolute maximum value among specified numbers.
average(,)	Returns the average value among specified numbers. E.g. Average(1,2,3)=2.
if(,,)	If(condition, TrueExpression, FalseExpression).If condition is true then TrueExpression is executer, otherwise FalseExpression.
switch(,,)	Returns switch(type, t1, expression1, .., tN, expressionN).If type = t1 then expression1 is executed.
exp()	Returns e raised to the specified power.
abs()	Returns the absolute value of a specified number.
sin()	Returns the sine of the specified angle.
cos()	Returns the cosine of the specified angle.
tan()	Returns the tangent of the specified angle.
log()	Returns the natural (base e) logarithm of a specified number.
round()	Rounds a value to the nearest integer or specified number of decimal places.
sign()	Returns a value indicating the sign of a number.
sinh()	Returns the hyperbolic sine of the specified angle.
cosh()	Returns the hyperbolic cosine of the specified angle.
tanh()	Returns the hyperbolic tangent of the specified angle.
asin()	Returns the angle whose sine is the specified number.
acos()	Returns the angle whose cosine is the specified number.
atan()	Returns the angle whose tangent is the specified number.
atan2(,)	Returns the angle whose tangent is the quotient of two specified numbers.
PI	Mathematical Constant = 3.14159.
Interpolate('Standard Table Alias with () brackets', 'X Column Number', 'Y Column Number', 'Input Value to find range from X Column'	Interpolates value of Y Column from the Standard Tables of the standard by setting X and Y column number and value at X column to get the interpolated value;

Material Variables

Name	Description
young	Young Modulus
poisson	Poisson Ratio
shearm	Shear Modulus
shear	Shear
mdensity	Mass Density
tensile	Tensile Strength
yield	Yield Stress

Property Variables

Name	Description
area	Area
nsm	Nonstructural mass
torsional	Torsional Constant
perimeter	Perimeter
coeff	Coefficient for Torsional Stress
tension	InitialTension
slack	Initial Slack
allow_stress	Allowable Tensile Stress
area_inertia	Area Moment of Inertia
inner	Inner Diametr
outer	Outer Diametr
pressure	Internal Pressure
izz	Moment of Inertia, Izz
iyy	Moment of Inertia, Iyy
izy	Moment of Inertia, Izy
yshear	Y Shear Area
zshear	Z Shear Area
warping	Warping Constrant
yneutral	Y Neutral Axis Offset
zneutral	Z Neutral Axis Offset
t1	Thickness 1
t2	Thickness 2
t3	Thickness 3
t4	Thickness 4
topfiber	Top Fiber
botfiber	Bottom Fiber
tshear	TShear/Mem Thickness
stiff	Bend Stiffness
DIM1	Cross section Dimension1 (or Height or Radius)
DIM2	Cross section Dimension2 (or Weight)
DIM3	Cross section Dimension3 (or Weight2)
DIM4	Cross section Dimension42 (or Thickness1)
DIM5	Cross section Dimension5 (or Thickness2)
DIM6	Cross section Dimension6 (or Thickness)
H	Cross section Height
R	Cross section Radius
W1	Cross section Width 1
W2	Cross section Width 2
TH1	Cross section Thickness 1
TH2	Cross section Thickness 2
T	Cross section Thickness
Shape Property	Cross Section Shape
stiffened_type	Get cross section stiffened type = {stiffened, unstiffened, combined}
WebThickness	Get Section Web Thickness
WebWidth	Get Section Web Width
WebWidth_NoFlanges	Get Section Web Width between flanges (minus flanges thicknesses)
WebArea	Get Section Web Area
FlangeTopThickness	Get Section top flange thickness
FlangeBottomThickness	Get Section bottom flange thickness
SDCSectionType	Get Section SDC Type (I,C,L,T, box or circle)
FlangeTopWidth	Get Section top flange width
FlangeBottomWidth	Get Section bottom flange width
ShapeYOrientation	Get Section Y Axis Orientation (Left, Right, Up or Down)
Cbot_Major	Get distance from bottom to neutral line for major axis
Cbot_Minor	Get distance from bottom to neutral line for minor axis
Ctop_Major	Get distance from top to neutral line for major axis
Ctop_Minor	Get distance from top to neutral line for minor axis
VerticalAxis	Get Vertical Axis (Y or Z axis oriented up and down in section)
Double_Symmetric	Get if shape is double symmetric
Section_Height	Get overall section height (calculated by SDC using point of interests)
Section_Width	Get overall section width (calculated by SDC using point of interests)
Imin	Principal Minimum Moment of Inertia, Imin
Imax	Principal Max Moment of Inertia, Imax
PrincipleAngle	Princple Angle
yc_top	Distance from centroid to the top fibre (along y axis)
yc_bot	Distance from centroid to the bottom fibre (along y axis)
yc_min	Min distance from centroid to the fibre (along y axis)
yc_max	Max distance from centroid to the fibre (along y axis)
zc_top	Distance from centroid to the top fibre (along z axis)
zc_bot	Distance from centroid to the bottom fibre (along z axis)
zc_min	Min distance from centroid to the fibre (along z axis)
zc_max	Max distance from centroid to the fibre (along z axis)
shapeydistance	Shape distance from bottom/left to the top/right (along y axis)
shapezdistance	Shape distance from bottom/left to the top/right (along z axis)

Results

Name	Description
S	Stress
S.x / S.y / S.z	Normal Stresses
S.xy / S.yz / S.zx	Shear Stresses
S.eqv	Equivalent / Von Mises Stress
Smin / Smax / Sabs / Sdelta	Min / Max / Abs / Delta Stress (for Load Group option only)
S[1] .. S[8]	Corner Stress
S[top] / S[bot] / S[total]	Absolute maximum stress for top corners / bottom corners / all

Similar as above variables can be used for the following result categories:

Name	Description
SWeld	Weld Stresses for shell elements. Original Stresses will be displayed for the rest of elements.
SWeld.X	Stress parallel to the weld direction
SWeld.Y	Stress perpendicular to the weld direction
SWeld.XY	Shear stress in weld direction
S_HotSpot	Hot Spot Stresses. Original Stresses or 0 (depends on the option defined in Job Settings of calculated load) will be displayed for the elements without hot spot locations defined.
SMat	Material Stresses for shell elements. Original Stresses will be displayed for the rest of elements.
SMidp	Mid-Plane Stresses for shell elements. Original Stresses will be displayed for the rest of elements.
SGlobalp	Global Plate Stresses for shell elements. Original Stresses will be displayed for the rest of elements. Equivalent direction cannot be used.
St	Strain
SPrin.Max / SPrin.Min / SPrin.Int / SPrin.MaxShear / SPrin.Angle	Max / Min / Int / Max Shear / Principal Angle of the Principal Stresses results;

Line Element Results

Name	Description
Mbend1 / Mbend2	Bending Plane Moment (local element plane XY / YZ)
Fshear1 / Fshear2	Shear Force 1 (local element plane XY / XZ)
Faxial	Axial Force
Ftorque	Torque Force
Fwarping_torque	Wapring Force
Faxial.Min / Faxial.Max / Faxial.Abs / Faxial. Delta	Min / Max / Abs / Delta Axial Force (for Load Group option only)
Faxial[top] / Faxial[bot]	Axial Force on start / end

Plate / Shell Element Results

Name	Description
FmembraneX / FmembraneY / FMembraneXY	Membrane Force X
MbendX / MbendY / MbendXY	Bending Moment X/Y/XY
FtransShearX / FTransShearY	Trans Shear Force X/Y
FmembraneX.Min / FmembraneX.Max / FmemberaneX.Abs	dMin / Max / Abs membrane force (for load group)
FmembraneX[1] .. FmembraneX[4]	Corner result for membrane force

Plate Buckling Results

Name	Description
Smidplane_Avg.X/Y/XY	Average midplane stress in X/Y/XY directions
Smidplane_Min.X/Y	Minimum midplane stress in X/Y directions
Smidplane_Abs.XY	Absolute Maximum midplane stress in XY direction
Splateaverage_elem_avg.X/Y/XY	Averaged Stress over buckling plate (Element Average Stress)
Splatemax_elem_avg.X/Y/XY	Max Stress over buckling plate (Element Average Stress)
Splatemin_elem_avg.X/Y/XY	Min Stress over buckling plate (Element Average Stress)

Plate Dimensions

Values obtained from Panel Finder Tool.

Name	Description
Plate.Length	Plate length
Plate.Width	Plate width
Plate.Thickness	Thickness of currently calculated element of the plate
Plate.ThicknessRatio	Ratio of user defined thickness to currently calculated element of the plate
Plate.C1	Coefficient C1 used in ABS Plate Buckling standards
Plate.C2	Coefficient C2 used in ABS Plate Buckling standards
Plate.PsiX	Coefficient PsiX used in DNV 1995 Plate Buckling standard
Plate.PsiY	Coefficient PsiY used in DNV 1995 Plate Buckling standard
Plate.L_W_Ratio	Plate length to width ratio
Plate.W_L_Ratio	Plate width to length ratio
Plate.HasFreeEdge	Check if plate has free edges

Weld Results

Results obtained from Weld Summation Tool.

Name	Description
Weld.Fx_Summed_Element	AbsMax force X on element from converted into averaged csys of the element corners
Weld.Fy_Summed_Element	AbsMax force Y on element from converted into averaged csys of the element corners
Weld.Fz_Summed_Element	AbsMax force XY on element from converted into averaged csys of the element corners
Weld.Mx_Summed_Element	AbsMax moment X on element from converted into averaged csys of the element corners
Weld.My_Summed_Element	AbsMax moment Y on element from converted into averaged csys of the element corners
Weld.Mz_Summed_Element	AbsMax moment XY on element from converted into averaged csys of the element corners

Weld Dimensions

Values obtained from Weld Finder Tool.

Name	Description
Weld.Length	Weld length
Weld.Element_Length	Weld length calculated by elemental method from weld summation tool
Weld.Part_Thickness	Plate thickness or minimum thickness of all walls of the beam
Weld.R	Weld leg horizontal
Weld.S	Weld penetration depth
Weld.H	Weld leg vertical
Weld.Thickness	Weld throat thickness
Weld.Type	Type of the weld. Can be compared with inner constants: WeldType_None, WeldType_DoubleFullPenetration, WeldType_DoublePartialPenetration, WeldType_DoubleFillet, WeldType_SingleFillet
Weld.Side	Side of the weld for Single Fillet weld type. Can be compared with inner constants: WeldSide_PlusY, WeldSide_MinusY

Stiffener Results

Results obtained from Effective Plate Width Tool.

Name	Description
Stiffener.Faxial	Axial Force in stiffener element
Stiffener.FaxialAvg	Average axial force
Stiffener.Psd	Design Lateral Pressure
Stiffener.Vsd	Shear Force in stiffener element
Stiffener.PlateSx	Averaged plate stresses of half of plates elements connected to the stiffener parallel to the stiffener
Stiffener.PlateSy	Averaged plate stresses of half of plates elements connected to the stiffener perpendicular to the stiffener
Stiffener.PlateSxy	Averaged plate shear stresses of half of plates elements connected to the stiffener
Stiffener.Se	Effective Stiffener Width

Stiffener Dimensions

Values obtained from Panel Finder Tool.

Name	Description
Stiffener.Length	Length of the stiffener
Stiffener.PlateAverageWidth	Averaged width of all connected plates to the stiffener
Stiffener.PlateMinThickness	Minimum plate thickness
Stiffener.Type	Continuous or snipped
Stiffener.PlateCount	Count of connected plates
Stiffener.IsCurved	Check is stiffener is curved
Stiffener.HasSameDirectionAndOrientation	Check if all elements in stiffener has same orientation

Connection Results

Results obtained from Braces Stress and Brace Classification tools. Following list of variables get result of the currently calculated brace. Same variables can be used from to get result from any brace of the connection by replacing BraceStress or Brace with Connection.Upper/Lower.Brace1/Brace2/Brace3 (e.g. Connection.Upper.Brace2.AxialForce will return axial force from the second upper brace of the connection).

Name	Description
BraceStress.AxialForce, Brace.AxialForce	Axial force of the brace
BraceStress.IPBMoment, Brace.IPBMoment	Bending moment in plane of connection of the brace
BraceStress.OPBMoment, Brace.OPBMoment	Bending moment out of plane of connection of the brace
BraceStress.AxialStress, Brace.AxialStress	Axial stress of the brace
BraceStress.IPBStress, Brace.IPBStress	Bending stress in plane of connection of the brace
BraceStress.OPBStress, Brace.OPBStress	Bending stress out of plane of connection of the brace
BraceStress.ChordAxialForceLeft, Brace.ChordAxialForceLeft	Axial force of the chord from the left element at Brace-Chord joint node
BraceStress.ChordAxialForceRight, Brace.ChordAxialForceRight	Axial force of the chord from the right element at Brace-Chord joint node
BraceStress.ChordAxialForceAverage, Brace.ChordAxialForceAverage	Average axial force of the chord at Brace-Chord joint node
BraceStress.IPBMomentLeft, Brace.IPBMomentLeft	Bending moment in plane of connection of the chord from the left element at Brace-Chord joint node
BraceStress.IPBMomentRight, Brace.IPBMomentRight	Bending moment in plane of connection of the chord from the right element at Brace-Chord joint node
BraceStress.IPBMomentAverage, Brace.IPBMomentAverage	Average bending moment in plane of connection of the chord at Brace-Chord joint node
BraceStress.OPBMomentLeft, Brace.OPBMomentLeft	Bending moment out of plane of the chord from the left element at Brace-Chord joint node
BraceStress.OPBMomentRight, Brace.OPBMomentRight	Bending moment out of plane of the chord from the right element at Brace-Chord joint node
BraceStress.OPBMomentAverage, Brace.OPBMomentAverage	Average bending moment out of plane of the chord at Brace-Chord joint node
BraceStress.ChordAxialStressLeft, Brace.ChordAxialStressLeft	Axial stress of the chord from the left element at Brace-Chord joint node
BraceStress.ChordAxialStressRight, Brace.ChordAxialStressRight	Axial stress of the chord from the right element at Brace-Chord joint node
BraceStress.ChordAxialStressAverage, Brace.ChordAxialStressAverage	Average axial stress of the chord at Brace-Chord joint node
BraceStress.IPBStressLeft, Brace.IPBStressLeft	Bending stress in plane of connection of the chord from the left element at Brace-Chord joint node
BraceStress.IPBStressRight, Brace.IPBStressRight	Bending stress in plane of connection of the chord from the right element at Brace-Chord joint node
BraceStress.IPBStressAverage, Brace.IPBStressAverage	Average bending stress in plane of connection of the chord at Brace-Chord joint node
BraceStress.OPBStressLeft, Brace.OPBStressLeft	Bending stress out of plane of the chord from the left element at Brace-Chord joint node
BraceStress.OPBStressRight, Brace.OPBStressRight	Bending stress out of plane of the chord from the right element at Brace-Chord joint node
BraceStress.OPBStressAverage, Brace.OPBStressAverage	Average bending stress out of plane of the chord at Brace-Chord joint node
BraceTypeLefToRight.K, Brace.BraceTypeKTotalForce	Percentage of K Type using Left-to-Right method
BraceTypeLefToRight.Ty, Brace.BraceTypeTyTotalForce	Percentage of TY Type using Left-to-Right method
BraceTypeLefToRight.Cross, Brace.BraceTypeCrossTotalForce	Percentage of Cross Type using Left-to-Right method
BraceTypeLefToRight.TotalGap, Brace.BraceTypeTotalGapTotalForce	Sum of all gaps multiplied on percentage of each that depends on the percentage of the taken load using Left-to-Right method
BraceTypeTotalForce.K, Brace.BraceTypeKLeftToRight	Percentage of K Type using Total Forces method
BraceTypeTotalForce.Ty, Brace.BraceTypeTyLeftToRight	Percentage of TY Type using Total Forces method
BraceTypeTotalForce.Cross, Brace.BraceTypeCrossLeftToRight	Percentage of Cross Type using Total Forces method
BraceTypeTotalForce.TotalGap, Brace.BraceTypeTotalGapLeftToRight	Sum of all gaps multiplied on percentage of each that depends on the percentage of the taken load using Total Forces method
Brace.IPShearForce	Shear force in plane of connection of the brace
Brace.OPShearForce	Shear force out of plane of connection of the brace
Brace.TorsionalMoment	Torsional moment of connection of the brace

Following list of variables get result from all the braces in the connection (e.g. summed or absmax axial force from all braces of the connection)

Name	Description
BraceStress.SumIPBMomentUpperBraces	Summed in plane bending moment from all upper braces of the connection
BraceStress.SumOPBMomentUpperBraces	Summed out of plane bending moment from all upper braces of the connection
BraceStress.SumAxialForceLowerBraces	Summed axial force from all lower braces of the connection
BraceStress.SumPerpendicularAxialForceLowerBraces	Summed axial force perpendicular to the chord from all lower braces of the connection
BraceStress.SumParallelAxialForceLowerBraces	Summed axial force parallel to the chord from all lower braces of the connection
BraceStress.SumIPBMomentLowerBraces	Summed in plane bending moment from all lower braces of the connection
BraceStress.SumOPBMomentLowerBraces	Summed out of plane bending moment from all lower braces of the connection
BraceStress.SumAxialStressUpperBraces	Summed axial stress from all upper braces of the connection
BraceStress.SumPerpendicularAxialStressUpperBraces	Summed axial stress (using axial force perpendicular to the chord) from all upper braces of the connection
BraceStress.SumParallelAxialStressUpperBraces	Summed axial stress (using axial force parallel to the chord) from all upper braces of the connection
BraceStress.SumIPBStressUpperBraces	Summed in plane bending stress from all upper braces of the connection
BraceStress.SumOPBStressUpperBraces	Summed out of plane bending stress from all upper braces of the connection
BraceStress.SumAxialStressLowerBraces	Summed axial stress from all lower braces of the connection
BraceStress.SumPerpendicularAxialStressLowerBraces	Summed axial stress (using axial force perpendicular to the chord) from all lower braces of the connection
BraceStress.SumParallelAxialStressLowerBraces	Summed axial stress (using axial force parallel to the chord) from all lower braces of the connection
BraceStress.SumIPBStressLowerBraces	Summed in plane bending stress from all lower braces of the connection
BraceStress.SumOPBStressLowerBraces	Summed out of plane bending stress from all lower braces of the connection
BraceStress.BraceAbsMaxForceParallel	Absolute maximum axial force parallel to the chord from all braces of the connection
BraceStress.BraceAbsMaxForcePerpendicular	Absolute maximum axial force perpendicular to the chord from all braces of the connection
BraceStress.ChordMinAxialForce	Minimum axial force of all chord elements
BraceStress.ChordMaxAxialForce	Maximum axial force of all chord elements
BraceStress.ChordAbsMaxAxialForce	Absolute Maximum axial force of all chord elements
BraceStress.ChordAbsMaxAxialForceInGap	Absolute maximum value of summed axial forces parallel to the chord of the chord element and all braces from the same side of the joint node

Connection Dimensions

Values obtained from Connection Finder Tool and additionally calculated values

Name	Description
Connection.Type	Return type of connection. Comparison in formulas can be done with inner constants: ConnectionType_CHS, ConnectionType_RHS, ConnectionType_IBeam, ConnectionType_Combined
Connection.IsBraceElement	Checks if currently calculated element of the connection belongs to braces
Connection.IsChordElement	Checks if currently calculated element of the connection belongs to chord
Connection.Upper	Access the variables of upper braces Brace1, Brace2, Brace3 of the connection
Connection.Lower	Access the variables of lower braces Brace1, Brace2, Brace3 of the connection
Connection.Upper.Brace1.CHS	Access the following results of the first upper brace of connection: Diameter, Thickness, L, L1, L2, Ov, Q. If brace is not circular shape or brace does not exist - 0 result is returned. Similarly, Brace2 and Brace3 can be used: Connection.Upper.Brace2.CHS, Connection.Upper.Brace3.CHS
Connection.Upper.Brace1.RHS	Access the following results of the first upper brace of connection: Height, Width, ThicknessMin, Ov, Q. If brace is not rectangular shape or brace does not exist - 0 result is returned. Similarly, Brace2 and Brace3 can be used: Connection.Upper.Brace2.RHS, Connection.Upper.Brace3.RHS
Connection.Upper.Brace1.IBeam	Access the following results of the first upper brace of connection: Height, Width, FlangeThicknessMin, WebThickness. If brace is not I-Beam shape or brace does not exist - 0 result is returned. Similarly, Brace2 and Brace3 can be used: Connection.Upper.Brace2.IBeam, Connection.Upper.Brace3.IBeam
Connection.Lower.Brace1.CHS	Access the following results of the first lower brace of connection: Diameter, Thickness, L, L1, L2, Ov, Q. If brace is not circular shape or brace does not exist - 0 result is returned. Similarly, Brace2 and Brace3 can be used: Connection.Lower.Brace2.CHS, Connection.Lower.Brace3.CHS
Connection.Lower.Brace1.RHS	Access the following results of the first lower brace of connection: Height, Width, ThicknessMin, Ov, Q. If brace is not rectangular shape or brace does not exist - 0 result is returned. Similarly, Brace2 and Brace3 can be used: Connection.Lower.Brace2.RHS, Connection.Lower.Brace3.RHS
Connection.Lower.Brace1.IBeam	Access the following results of the first lower brace of connection: Height, Width, FlangeThicknessMin, WebThickness. If brace is not I-Beam shape or brace does not exist - 0 result is returned. Similarly, Brace2 and Brace3 can be used: Connection.Lower.Brace2.IBeam, Connection.Lower.Brace3.IBeam
GapToCurrentBrace	Gap distance (negative value for overlapping) from one of the braces to currently calculated brace. Can be accessed for following braces: Connection.Upper.Brace1, Connection.Upper.Brace2, Connection.Upper.Brace3, Connection.Lower.Brace1, Connection.Lower.Brace2, Connection.Lower.Brace3
EccentricityWithCurrentBrace	Get eccentricity value from one of the braces with currently calculated brace. Can be accessed for following braces: Connection.Upper.Brace1, Connection.Upper.Brace2, Connection.Upper.Brace3, Connection.Lower.Brace1, Connection.Lower.Brace2, Connection.Lower.Brace3
IsOverlappingForCurrentBrace	Checks if one of the braces is overlapping with currently calculated brace. Can be accessed for following braces: Connection.Upper.Brace1, Connection.Upper.Brace2, Connection.Upper.Brace3, Connection.Lower.Brace1, Connection.Lower.Brace2, Connection.Lower.Brace3
Connection.SumBracesHeights	Summed height (cross section size in plane of connection) of all the braces of the connection
Connection.SumBracesHeightsUpper	Summed height of all upper braces of the connection
Connection.SumBracesHeightsLower	Summed height of all lower braces of the connection
Connection.SumBracesWidths	Summed width (cross section size out of plane of connection) of all the braces of the connection
Connection.SumBracesWidthsUpper	Summed width of all upper braces of the connection
Connection.SumBracesWidthsLower	Summed width of all lower braces of the connection
Connection.BracesCount	Amount of all braces of the connection
Connection.UpperBracesCount	Amount of upper braces of the connection
Connection.LowerBracesCount	Amount of lower braces of the connection
Chord.Type	Return type of the chord. Comparison in formulas can be done with inner constants: ChordType_CHS, ChordType_RHS, ChordType_IBeam
ChordCHS.Diameter	Maximum diameter of all chord CHS elements if Can is found or minimum diameter otherwise
ChordCHS.NominalDiameter	Minimum diameter of all chord CHS elements
ChordCHS.NominalThickness	Minimum thickness of all chord CHS elements
ChordCHS.CanThickness	Maximum thickness of all chord CHS elements if Can is found or minimum thickness otherwise
ChordCHS.ContainsCan	Checks if chord contains Can for CHS cross sections
ChordCHS.NominalYieldStress	Yield Stress of the CHS element of the chord with minimum thickness
ChordCHS.NominalTensileStrength	Tensile Strength of the CHS element of the chord with minimum thickness
ChordRHS.Height	Minimum height in plane of connection of all chord RHS elements
ChordRHS.Width	Minimum width out of plane of connection of all chord RHS elements
ChordRHS.ThicknessMin	Minimum thickness of all chord RHS elements
ChordIBeam.Height	Minimum height in plane of connection of all chord I-Beam elements
ChordIBeam.Width	Minimum width out of plane of connection of all chord I-Beam elements flanges
ChordIBeam.FlangeThicknessMin	Minimum flange thickness of all chord I-Beam elements
ChordIBeam.WebThickness	Minimum web thickness of all chord I-Beam elements
Brace.Type	Return type of the currently calculated brace. Comparison in formulas can be done with inner constants: BraceType_CHS, BraceType_RHS, BraceType_IBeam
Brace.ElementId	Element ID of the currently calculated brace
Brace.Height	Cross section height (size in plane of connection) of the currently calculated brace
Brace.Width	Cross section width (size out of plane of connection) of the currently calculated brace
Brace.Number	Number of brace in the connection of the currently calculated brace
Brace.NumberUpper	Number of the upper brace in the connection of the currently calculated brace. Return 0 if current brace is lower
Brace.NumberLower	Number of the lower brace in the connection of the currently calculated brace. Return 0 if current brace is upper
Brace.IsUpper	Checks if currently calculated brace is upper
Brace.IsLower	Checks if currently calculated brace is lower
Brace.IsOverlapping	Checks if currently calculated brace is overlapping
Brace.Angle	Angle of currently calculated brace to the chord in degrees. Range is [0; 90]
Brace.EffectiveLength	Effective Length (distance from the brace to the end of chord Can) of currently calculated brace for CHS connections if Can is found
Brace.Yield	Yield Stress of currently calculated brace
Brace.Tensile	Tensile Strength of currently calculated brace
Brace.Young	Young's Modulus of currently calculated brace
Brace.IsDifferentChordPropertyAtJoint	Checks if chord has different property sizes of the chord at the Brace-Chord joint node
Brace.ChordYieldStressAtJointLeft	Yield Stress of the left element of the chord at the Brace-Chord joint node
Brace.ChordYieldStressAtJointRight	Yield Stress of the right element of the chord at the Brace-Chord joint node
Brace.ChordYieldStressAtJointAverage	Average Yield Stress of the of the chord elements at the Brace-Chord joint node
Brace.ChordTensileStrengthAtJointLeft	Tensile Strength of the left element of the chord at the Brace-Chord joint node
Brace.ChordTensileStrengthAtJointRight	Tensile Strength of the right element of the chord at the Brace-Chord joint node
Brace.ChordTensileStrengthAtJointAverage	Average Tensile Strength of the of the chord elements at the Brace-Chord joint node
Brace.ChordYoungAtJointLeft	Young's Modulus of the left element of the chord at the Brace-Chord joint node
Brace.ChordYoungAtJointRight	Young's Modulus of the right element of the chord at the Brace-Chord joint node
Brace.ChordYoungAtJointAverage	Average Young's Modulus of the of the chord elements at the Brace-Chord joint node
BraceCHS.Thickness	Thickness of currently calculated CHS brace
BraceCHS.Diameter	Diameter of currently calculated CHS brace
BraceCHS.L	Thickness of currently calculated CHS brace
BraceCHS.L1	Thickness of currently calculated CHS brace
BraceCHS.L2	Thickness of currently calculated CHS brace
BraceCHS.Ov	Thickness of currently calculated CHS brace
BraceCHS.Q	Thickness of currently calculated CHS brace
BraceRHS.Height	Height of currently calculated RHS brace in plane of connection
BraceRHS.Width	Height of currently calculated RHS brace out of plane of connection
BraceRHS.ThicknessMin	Minimum thickness of currently calculated RHS brace
BraceIBeam.Height	Height of currently calculated I-Beam brace in plane of connection
BraceIBeam.Width	Width of currently calculated I-Beam brace out of plane of connection
BraceIBeam.FlangeThicknessMin	Minimum flange thickness of currently calculated I-Beam brace
BraceIBeam.WebThickness	Web thickness of all chord I-Beam elements

The following functions can be also used to obtain results between two braces of connection:

Name	Description
GapBetweenBracesUpper(br1, br2)	Calculate geometrical distance between two upper braces of connection on the chord shell. Br1, Br2 - numbers of upper brace in connection.
GapBetweenBracesLower(br1, br2)	Calculate geometrical distance between two lower braces of connection on the chord shell. Br1, Br2 - numbers of lower braces in connection.
AngleBetweenBracesUpper(br1, br2)	Angle between two upper braces in radians. Br1, Br2 - numbers of upper brace in connection.
AngleBetweenBracesLower(br1, br2)	Angle between two lower braces in radians. Br1, Br2 - numbers of lower brace in connection.

Beam Member Results

Results of Moment Ratio Tool

Variable	Value
Tool.MaxMomentY, MemberY.MaxMoment	Max moment over member in Y direction.
Tool.MaxMomentZ, MemberZ.MaxMoment	Max moment over member in Z direction
MemberTorsional.MaxMomentY, MemberTorsional.MaxMomentZ	Max moment over torsional member in Y/Z direction
MemberY.MaxPrinMoment, MemberZ.MaxPrinMoment	Max principal moment over member in Y/Z direction
MemberTorsional.MaxPrinMomentY, MemberTorsional.MaxPrinMomentZ	Max principal moment over torsional member in Y/Z direction
MemberY.MaxMomentOnEnd, MemberZ.MaxMomentOnEnd	Max moment of member ends in Y/Z direction
MemberTorsional.MaxMomentOnEndY, MemberTorsional.MaxMomentOnEndZ	Max moment of torsional member ends in Y/Z direction
MemberY.MaxPrinMomentOnEnd, MemberZ.MaxPrinMomentOnEnd	Max principal moment of member ends in Y/Z direction
MemberTorsional.MaxPrinMomentOnEndY, MemberTorsional.MaxPrinMomentOnEndZ	Max principal moment of torsional member ends in Y/Z direction
MemberY.IsMaxMomentOnEnd, MemberZ.IsMaxMomentOnEnd	Checks if max moment of full member is located at member ends in Y/Z direction
MemberTorsional.IsMaxMomentOnEndY, MemberTorsional.IsMaxMomentOnEndZ	Checks if max moment of torsional member is located at member ends in Y/Z direction
MemberY.IsMaxPrinMomentOnEnd, MemberZ.IsMaxPrinMomentOnEnd	Checks if max principal moment of member is located at member ends in Y/Z direction
MemberTorsional.IsMaxPrinMomentOnEndY, MemberTorsional.IsMaxPrinMomentOnEndZ	Checks if max principal moment of torsional member is located at member ends in Y/Z direction
Tool.MinMomentY, MemberY.MinMoment	Min moment over member in Y direction
Tool.MinMomentZ, MemberZ.MinMoment	Min moment over member in Z direction
MemberTorsional.MinMomentY, MemberTorsional.MinMomentZ	Min moment over torsional member in Y/Z direction
MemberY.MinPrinMoment, MemberZ.MinPrinMoment	Min principal moment over member in Y/Z direction
MemberTorsional.MinPrinMomentY, MemberTorsional.MinPrinMomentZ	Min principal moment over torsional member in Y/Z direction
MemberY.MinMomentOnEnd, MemberZ.MinMomentOnEnd	Min moment of member ends in Y/Z direction
MemberTorsional.MinMomentOnEndY, MemberTorsional.MinMomentOnEndZ	Min moment of torsional member ends in Y/Z direction
MemberY.MinPrinMomentOnEnd, MemberZ.MinPrinMomentOnEnd	Min principal moment of member ends in Y/Z direction
MemberTorsional.MinPrinMomentOnEndY, MemberTorsional.MinPrinMomentOnEndZ	Min principal moment of torsional member ends in Y/Z direction
Tool.M1M2Ratio_Y, MemberY.M1M2RatioOnEnd	Moment ratio over member ends in Y direction
Tool.M1M2Ratio_Z, MemberZ.M1M2RatioOnEnd	Moment ratio over member ends in Z direction
Tool.M1M2RatioTorsionalY, MemberTorsional.M1M2RatioOnEndZ	Moment ratio over torsional member ends in Y/Z direction
MemberY.M1M2PrinRatioOnEnd, MemberZ.M1M2PrinRatioOnEnd	Principal moment ratio over member ends in Y/Z direction
MemberTorsional.M1M2PrinRatioOnEndY, MemberTorsional.M1M2PrinRatioOnEndZ	Principal moment ratio over torsional member ends in Y/Z direction
Tool.Kc_Y, MemberY.Kc	Kc coefficient (Eurocode3) of member in Y direction
Tool.Kc_Z, MemberZ.Kc	Kc coefficient (Eurocode3) of member in Z direction
MemberTorsional.KcY, MemberTorsional.KcZ	Kc coefficient (Eurocode3) of torsional member in Y/Z direction
MemberY.KcPrin, MemberZ.KcPrin	Kc coefficient (Eurocode3) of member in Y/Z direction using moments in principal axes
MemberTorsional.KcPrinY, MemberTorsional.KcPrinZ	Kc coefficient (Eurocode3) of torsional member in Y/Z direction using moments in principal axes
Tool.CbY, MemberTorsional.Cby_Aisc2010	Cb coefficient (AISC 360-10) of torsional member in Y direction
Tool.CbZ, MemberTorsional.Cbz_Aisc2010	Cb coefficient (AISC 360-10) of torsional member in Z direction
MemberTorsional.CbPriny_Aisc2010, MemberTorsional.CbPrinz_Aisc2010	Cb coefficient (AISC 360-10) of torsional member in Y/Z direction using moments in principal axes
Tool.CbY_AISC89, MemberTorsional.Cby_Aisc89	Cb coefficient (AISC 89) in Y direction
Tool.CbZ_AISC89, MemberTorsional.Cbz_Aisc89	Cb coefficient (AISC 89) in Z direction
MemberTorsional.CbPriny_Aisc89, MemberTorsional.CbPrinz_Aisc89	Cb coefficient (AISC 89) of torsional member in Y/Z direction using moments in principal axes
MemberY.BetaM, MemberZ.BetaM	Bm coefficient (Eurocode3 Fire Design) of member in Y/Z direction
MemberTorsional.BetaMY, MemberTorsional.BetaMZ	Bm coefficient (Eurocode3 Fire Design) of member in Y/Z direction
MemberY.BetaMPrin, MemberZ.BetaMPrin	Bm coefficient (Eurocode3 Fire Design) of member in Y/Z direction
MemberTorsional.BetaMPrinY, MemberTorsional.BetaMPrinZ	Bm coefficient (Eurocode3 Fire Design) of member in Y/Z direction

Beam Member Dimensions

Values obtained from Beam Member Finder Tool

Variable	Value
MemberY.L	Length in Y direction
MemberY.K	Effective Length Factor in Y direction
MemberY.CmType	Cm Type in Y direction
MemberZ.L	Length in Z direction
MemberZ.K	Effective Length Factor in Z direction
MemberZ.CmType	Cm Type in Z direction
MemberTorsion.L	Length in torsional direction
MemberTorsion.K	Effective Length Factor in torsional direction
MemberTorsion.CmType	Cm Type in torsional direction

Rainflow Counting Variables

Results of Rainflow Counting Tool from the calculated iteration that is based on selected Category and Method in the Rainflow Summation Check.

Variable	Value
Rainflow.From	Start value of the calculated range
Rainflow.To	End value of the calculated range
Rainflow.Range	Calculated range value
Rainflow.Cycles	Number of the repeated cycles of the calculated range
Rainflow.Min	Minimum value of From and To
Rainflow.Max	Maximum value of From and To
Rainflow.Abs	Absolute Maximum value of From and To

Other Variables

Variable	Value
ShapeCircularTube.D	Diameter
ShapeCircularTube.Dinner	Diamter - 2 * thicknesses
ShapeCircularTube.R	Radius
ShapeCircularTube.Rinner	Radius - thickness
ShapeCircularTube.T	Thickness
ShapeCircularTube.ZY	Plastic Section Modulus in Y direction
ShapeCircularTube.ZZ	Plastic Section Modulus in Z direction
ShapeRectangularTube.H	Height (Rectangular Tube)
ShapeRectangularTube.Hw	Height - 2 * thicknesses
ShapeRectangularTube.B	Width
ShapeRectangularTube.TVertical	Vertical side thickness
ShapeRectangularTube.THorizontal	Horizontal side thickness
ShapeRectangularTube.TLeft	Left side thickness
ShapeRectangularTube.TRight	Right side thickness
ShapeRectangularTube.TTop	Top side thickness
ShapeRectangularTube.TBottom	Bottom side thickness
ShapeRectangularTube.ZY	Plastic Section Modulus in Y direction
ShapeRectangularTube.ZZ	Plastic Section Modulus in Z direction
ShapeC.H	Height (Channel)
ShapeC.Hw	Height - 2 * thicknesses
ShapeC.BMin	Min Width {Top, Bottom}
ShapeC.BTop	Top Width
ShapeC.BBottom	Bottom Width
ShapeC.TWeb	Web Thickness
ShapeC.TFlangeMin	Min Flange Thickness {Top, Bottom}
ShapeC.TFlangeTop	Flange Top Thickness
ShapeC.TFlangeBottom	Flange Bottom Thickness
ShapeC.ZY	Plastic Section Modulus in Y direction
ShapeC.ZZ	Plastic Section Modulus in Z direction
ShapeI.H	Height (I-beam)
ShapeI.Hw	Height - 2 * thicknesses
ShapeI.BMin	Min Width {Top, Bottom}
ShapeI.BTop	Top Width
ShapeI.BBottom	Bottom Width
ShapeI.TWeb	Web Thickness
ShapeI.TFlangeMin	Min Flange Thickness {Top, Bottom}
ShapeI.TFlangeTop	Flange Top Thickness
ShapeI.TFlangeBottom	Flange Bottom Thickness
ShapeI.HBRatio	Height / Width
ShapeI.ZY	Plastic Section Modulus in Y direction
ShapeI.ZZ	Plastic Section Modulus in Z direction
ShapeT.H	Full height (T-beam)
ShapeT.B	Width (T-beam)
ShapeT.Tweb	Web thickness (height)
ShapeT.Tflange	Flange thickness (width)
ShapeT.Y0	Centroid Y
ShapeT.Z0	Centroid Z
ShapeL.H	Height - bigger leg (L-beam)
ShapeL.B	Width - smaller leg (L-beam)
ShapeL.Th	Thickness of bigger leg
ShapeL.Tb	Thickness of smaller leg
ShapeL.Y0	Centroid Y
ShapeL.Z0	Centroid Z
Load.Sf	Load Safety Factor
Element.CenterX	Get average X coordinate from all the nodes of the element
Element.CenterY	Get average Y coordinate from all the nodes of the element
Element.CenterZ	Get average Z coordinate from all the nodes of the element
Element.IsLine	Check if element is 1D (e.g. beam)
Element.IsPlane	Check if element is 2D (e.g. shell/plate)
Element.IsVolume	Check if element is 3D (e.g. solid/volume)
Element.IsHotSpotCalculated	Check if hot spot is calculated for current point of interest of the element.
Element.IsHotSpotCalculated[1]..Element.IsHotSpotCalculated[8]	Check if hot spot is calculated for specified point of interest of the element.