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#b } • x "  B /q  ~  Š ˜ Ÿ ˛ :ě H4 -a h } œ %Á *ë    ( @ ^ž ľ >ó    ! ) C ` "‚  ˘   Ú $ţ -A1r0˘ş0ę7!<]<™5Î5585m4Ą4Ő4 4=Sekov} ‡›Ťą ź Ĺ Î8 + 4;@H Rh‚‰œłČŘí$->)g1˜&ž2đ$6H1y˜Ş2Ü÷3*(R&x9ąDőF;cž@ŢC!+L.z6°6ć88V5‹5Ŕ7÷7.@n2 ?ß* %.8f+‘6Ç$ë&):R _. —Šť&áËďModel1 End releasesSplit Active WindowResize Active Window Creates nodes Create LineDisplayPerspective SettingsManaging Parts!Managing Section Lines and Planes TranslateRotateMirrorScale IntersectGeometry CheckDefine ReferenceDefine Reference PointDefine Reference VectorDefine Reference AxisDefine Reference Plane Find SurfacesDefine Surface ElementModify Surface ElementsDefine Line ElementModify Line ElementsOverwrite Degrees of FreedomMerge Degrees of Freedom Define SpringModify Springs Define Gap Modify GapDefine SupportModify SupportsDefine Rigid ElementApply Nodal LoadsModify Nodal LoadsModify Load Cases!Apply Concentrated Loads to Beams"Modify Concentrated Loads on Beams%Apply Distributed Loads to Beams/Ribs&Modify Distributed Loads on Beams/Ribs)Apply Thermal Loads to Trusses/Beams/Ribs*Modify Thermal Loads on Trusses/Beams/Ribs&Apply Fault in Length to Trusses/Beams'Modify Fault in Length on Trusses/BeamsApply Tension to Trusses/BeamsModify Tension on Trusses/Beams+Apply Distributed Loads to Surface Elements,Modify Distributed Loads on Surface Elements$Apply Edge Loads to Surface Elements%Modify Edge Loads on Surface Elements'Apply Thermal Loads to Surface Elements(Modify Thermal Loads on Surface Elements"Apply Fluid Loads to Plates/Shells*Apply Influence Line Load to Trusses/BeamsModify Nodal MassApply Nodal Mass Edit TableReinf. ParametersArchiCad Static ModelDeleting ArchiCad ObjectsApply Self WeightDelete ReinforcementNew Reinforcement by Coord.New Reinforcement on CCDistribute ReinforcementsShift ReinforcementApply Support DisplacementModify Support Displacements Importing DXF Importing AXS Importing STLPlace Cross-SectionTranslate Cross-SectionRotate Cross-SectionMirror Cross-SectionAdd Stress Calculation PointDelete Stress Calculation PointDelete Cross-Section Define Link Modify LinkReinforcement for Crack ControlCreate Closed RegionChange Design CodeSeismic ParametersHorizontal GuidelineVertical GuidelineDouble GuidelineOblique GuidelineOblique Double GuidelineGuideline SetupGuideline Move Arc by CenterArc by Three PointsDefine Domains Define HolesModify Domain Parameters Generate MeshSteel Design ParametersChanging Rebar DiameterDelete Outside RebarsEditing reportOrthogonal dimension line(Modify orthogonal/aligned dimension lineAligned dimension lineAngle dimensionModify angle dimension Level symbolModify level/elevation symbolElevation symbolText boxModify text boxResult text boxModify result text box Opening model Saving modelERead-only file|The file to open is read only. Do you want to open it?,This model was created with a Trial Version./This model was created with a previous version.1Do you want to convert it to the present version?Interrupt analysis? Continue?Continue analysis? Overwrite? Nodal DOFOpening model...Opening undo file... Saving...Saving undo file...(Converting %s from Version 3.0 to 3.5...(Converting %s from Version 3.5 to 3.6...)Converting %s from Version 3.6 to 4.0...(Converting %s from Version 4.0 to 5.0...(Converting %s from Version 5.0 to 6.0....Converting %s from Version 6.0 R3 to 6.0 R4...-Converting %s from Version 6.0 R10 to 7.0 ...0Converting %s from Version 6.0 R4 to 6.0 R10 ...(Converting %s from Version 6.0 to 5.0....Converting %s from Version 6.0 R4 to 6.0 R3.../Converting %s from Version 6.0 R10 to 6.0 R4...,Converting %s from Version 7.0 to 6.0 R10...(Converting %s from Version 5.0 to 4.0...(Converting %s from Version 4.0 to 3.6...(Converting %s from Version 3.6 to 3.5...(Converting %s from Version 3.5 to 3.0...Removing hidden lines...Sorting lines for display...Creating/modifying nodesPreparing for optimization...Optimizing equations...Listing topology...Writing model data to disk...Deleting lines...Dividing lines...Listing rigid elements...Checking line elements...Checking surface elements...Checking domains...Checking supports...Dividing surface elements...L equal anglesL unequal anglesIPE European I-beamsIPN European standard beamsHE European wide flange beams HL beams with very wide flangesHD wide flange columnsHP wide flange bearing piles UB British universal columnsUC British universal columns"UAP channels with parallel flangesUPN European standard channels"[] Concrete square cross-sections!O Concrete round cross-sectionsO Hungarian pipes$O Hungarian steel rod round shapes'[] Hungarian cold formed square shapes,[] Hungarian cold formed rectangular shapesI Hungarian I-beamsU Hungarian standard channelsL Hungarian equal anglesL Hungarian unequal anglesI Romanian I-beamsU Romanian channelsL Romanian equal anglesL Romanian unequal angles O Dunaújvárosi Hungarian pipes'L Dunaújvárosi Hungarian equal angles)L Dunaújvárosi Hungarian unequal angles-[] Dunaújvárosi Hungarian rectangular shapes([] Dunaújvárosi Hungarian square shapes#C Dunaújvárosi Hungarian C shapes#U Dunaújvárosi Hungarian channels#Z Dunaújvárosi Hungarian Z shapes#S Dunaújvárosi Hungarian S shapes#J Dunaújvárosi Hungarian J shapes[] RHS square shapes[] RHS rectangular shapes AISC S Shapes AISC M ShapesAISC HP ShapesAISC Square TubingAISC Rectangular Tubing AISC S Pipes AISC ES PipesAISC DES PipesAISC Miscellaneous ChannelsAISC Standard Channels AISC Angles AISC W ShapesNEN round shapesNEN square shapes AxisVM 6.0Inter-CAD Kft.Š Inter-CAD Kft., 1991-20026.0 Registered toOKCancelDeletePress to cancelSuspendContinuePick UpDefineModify ReferenceType Direction%s has a maximum of %sGlobalLocal ReferentialXYZXXYYZZDXDYDZLabdrRhxyzDisplayLocal x ReferenceLocal z Reference?Conditions of use of this software can be found in LICENSE.TXT.GYou should read this file before using the software for the first time. ConfigurationAdd-On Modules Release %s Allow Changes Draws lines Divides linesHorizontal Division"Inserts a horizontal division lineVertical Division Inserts a vertical division line'Creates nodes at intersections of linesDivides a polygon$Moves/copies entities by translation!Moves/copies entities by rotation"Moves/copies entities by mirroring Moves/copies entities by scalingGeometry Check?Checks the geometry and deletes redundant or erroneous entitiesSearches for surfacesCreates a new modelOpens a model fileSaves the current modelPrint...Print from file...UndoRedo Selection8Sets selection mode to add entities to the selection setSymbolsGraphic symbols3Plane X-Z|Displays the model projected to Plane X-Z3Plane Y-Z|Displays the model projected to Plane Y-Z3Plane X-Y|Displays the model projected to Plane X-YMThree planes & perspective|Displays global plane views and a perspective viewSets/selects section linesSets/selects parts Weight ReportDisplays a weight reportFindFinds entities by indexDisplays model information(Renders a realistic 3D view of the model Draws linesDraws polylinesDraws rectanglesDraws skewed rectangles Quad DivisionDivides quads into quadsDivides quads into trianglesTriangle Division*Divides triangles into quads and triangles Divides triangels into triangles"Specifies properties for materials'Specifies properties for cross-sectionsCreates reference pointsCreates reference vectorsCreates reference planes Nodal DOFSets nodal degrees of freedom-Defines/modifies truss, beam and rib elements!Defines/modifies surface elementsDefines rigid elementsRecord|Compiles an animationStarts|Plays an animation Step forward|Displays next frame!Step back|Displays previous frameStops|Plays animationSuspends|Resumes animation6Concentrated|Applies concentrated loads to nodes/beams6Distributed|Applies distributed loads to beam elements9Distributed|Applies distributed loads to surface elements7Edge|Applies distributed edge loads to surface elements.Thermal Load|Applies thermal loads to elements5Length|Applies fault in length to beam/truss elementsFSupport Displacement|Applies a forced displacement to support elements7Fluid loads|Applies fluid loads to plate/shell elementsCSelf Weight|Applies (includes) self weight to the selected elementsOptionsESets preferences for grid, cursor, editing, drawing, and design codesCreates reference axes Nodal Loads Applies and modifies nodal loads0Applies and modifies concentrated loads to beamsConcentrated Loads on BeamsLoad Along Line Elements;Applies and modifies distributed loads to beam/rib elementsSurface Edge Loads&Applies edge loads to surface elementsDistributed Surface Load-Applies distributed loads to surface elementsPUniform Thermal Load|Select elements you want to apply a uniform thermal load to;Thermal Load on Line|Applies thermal loads to line elementsAThermal Load on Surface|Applies thermal loads to surface elementsTension/Compression,Applies tension/compression to line elementsFault in Length.Applies fault in length to beam/truss elementsInfluence Line1Applies influence line load to beam/truss element Seismic Load&Specifies parameters for seismic loads Perpendicular"Applies a perpendicular constraintParallelApplies a parallel constraintZoom OutZoom In4Performs a zoom out by defining a rectangular region3Performs a zoom in by defining a rectangular region?Fit in window|Scales the view to fit model in the active windowPanPans the drawing by a vector$View undo|Restores the previous view.View redo|Redoes the last view that was undone.Vibration Analysis|Starts a vibration analysis.Vibration Analysis|Starts a vibration analysis,Buckling Analysis|Starts a buckling analysis)Displays model data and results in tables!Redraws the content of the window Nodal Mass=Defines/modifies nodal mass on nodes by its global componentsArchiCAD Model`Sets display options for ArchiCAD Layer objects, deletes selected objects or creates a frameworkArc4Draws an arc based on centerpoint and two arc points&Draws an arc based on three arc pointsDomain meshingDomainHoleMeshDefines domains by selectionDefines holes by selection$Generates finite element domain mesh GuidelinesPlaces guidelinesDimension LinesPlaces dimension lines < mixed >WSaves an image of current window pane or all panes to the Gallery to use it in reports. Enter a nodeEnter line start pointEnter line end pointEnter polyline start pointEnter next polyline vertex'Enter a corner of the region to zoom inComplete the zoom rectangle(Enter a corner of the region to zoom out#Enter translation vector base point"Enter translation vector end pointNot enough memory(AxisVM has detected an application errorAccess violationString conversion errorFile read/write errorDivision by zeroInvalid integer value. Floating point error/OLE error: The object property is set read only0OLE error: The object property is set write onlyStack overflowVariant type handling errorThe file cannot be opened.Insufficient disk spaceSwapfile error|File not foundNot enough file handles (< 20)Data block missingError in SwapFile handler(File open error|The file is already open5File save error|The file cannot be opened for writing5File conversion error|This is not a valid AxisVM file@File conversion error|The model was created with a later version"Hardware lock invalid or not found%Key file not found in program folder.ZKey file %s is invalid. It may belong to another hardware lock or another program version.Unauthorized UserInvalid registered user name"Program use authorization expired!+Contact your dealer for further information"Error in the cross-section library(Nodes cannot be defined in graphics modeNode already existsUnattached point/node: Node %1d.Unknown constraint|The cursor is in the originNo nodes definedNo lines definedNo elements defined!Seismic loads cannot be generated%Seismic load parameters not specified9Too many load cases. Maximum number of load cases is %1d.+Too many elements. /Small Business Version/.Too many elements. /Educational Version (EDU)/No defined material#No cross-section properties defined-%s cross-section has a zero moment of inertia.Cross-section %s has a zero Hy and/or Hz valueNo load definedNo mass definedNo support element defined&Some definitions of DOF may be invalidCannot specify constraintsIndefinite point coordinatesEntity cannot be identifiedKInvalid command|All surface element edges belong to the same rigid element.BInvalid setting|The DOF of a node of rigid element may not be set. Invalid value Invalid nameWarning'Cannot copy to clipboard more than 16MB_Cannot create or write the following key in the Registry: HKEY_CURRENT_USER\Software\InterCAD".\AxisVM can run without it but certain custom settings (colors, fonts, etc.) cannot be saved.0Check your level of access on the Control Panel.File Creation ErrorCannot create %s.3Check if you have tried to run the program from CD.File already exists:File %s already exists in the target folder. Overwrite it? Delete %s?Delete %s from the Gallery?,Delete all unused pictures from the Gallery?Nodes Midside nodesLinesTrussesBeamsRibsSurfaces MembranesMembranes (plane strain)Membranes (plane stress)PlatesShellsSupportsRigidsSpringsGapsLinks Load Cases Load GroupsLoad Combinations Materials Cross-SectionMasses Section Lines PerspectivesPartsNodeDOF Midside nodeLinePolygon RectangleSkewed rectangleSectorRingTrussBeamRibSurfaceMembranemembraneMembrane (plane strain)Membrane (plane stress)PlateplateShellshellSupportRigidSpringGapLinkMass Load Case Load Group CombinationMaterial Cross-SectionLcLc.#%dCo.#%dMode %dReference PointReference Vector Reference AxisReference PlanePointVectorAxisPlaneGLeXeYeZfXfYfZeRfRexeyezfxfyfzNxQyQzMxMyMzSminSmaxSminmaxTymeanTzmeannxnynxymxmymxyqxzqyzqRzn1n2anm1m2amnxDnyDmxDmyDdnxdnydnxydmxdmydmxydqxdqySxxSyySxySxzSyzSVMS1S2aSSxx TSyy TSxy TSxz TSyz TSVM TS1 TS2 TaS TSxx CSyy CSxy CSxz CSyz CSVM CS1 CS2 CaS CSxx BSyy BSxy BSxz BSyz BSVM BS1 BS2 BaS BPX`1`PY`1`PZ`1`RxRyRzRxxRyyRzzRrRrrRxRyRzRxxRyyRzzRrRrraxbaybaxtaytaxb,axtayb,aytxbybxtytxb,xtyb,ytam(b)am(t)ame(b)ame(t)aR(b)aR(t)sxbsybsxtsytsxb,sxtsyb,sytExEyminmaxMinMaxAxial Force-Bending-ShearN-M-V%Compression-Bending-Flexural Buckling N-M-FlxBuckl.Compression-Bending-Lateral Torsional Buckling N-M-LTBuckl Shear (y)Vy Shear (z)VzWeb Shear-Bending-Axial ForceVw-M-NAxial Plastic ResistanceNplRdShear Resistance (y)VplyRdShear Resistance (z)VplzRdShear Web Buckling ResistanceVbaRdElastic Moment Resistance (yy)MelyRdElastic Moment Resistance (zz)MelzRdPlastic Moment Resistance (yy)MplyRdPlastic Moment Resistance (zz)MplzRd!Flexural Buckling Resistance (yy)NbyRd!Flexural Buckling Resistance (zz)NbzRd%Lateral-Torsional Buckling ResistanceMbRdAxial Force-Bending-ShearN-M-QCompression-Bending-Buckling N-M-Buckl.Compression-Bending-Lateral Torsional Buckling N-M-LTBuckl Shear (y)Qy Shear (z)Qz)Stress Resultant in the Web at the FlangeSr Web BucklingBkl-wFlange BucklingBkl-fAxial ResistanceNHShear Resistance (y)QyHShear Resistance (z)QzHMoment Resistance (yy)MyHMoment Resistance (zz)MzHBuckling Resistance (yy)NkiyHBuckling Resistance (zz)NkizH%Lateral-Torsional Buckling ResistanceMkHAxial Force-Bending-ShearN-M-V%Compression-Bending-Flexural Buckling N-M-FlxBuckl.Axial Force-Bending-Lateral Torsional Buckling N-M-LTBucklShearVAxial ResistanceNudShear Resistance (y)VyuRdShear Resistance (z)VzuRdMoment Resistance (yy)MyuRdMoment Resistance (zz)MzuRdBuckling Coefficient (y)obyBuckling Coefficient (z)obzC1C1C2C2&Lateral-Torsional-Buckling CoefficientoLTBAxial Force-Bending (strength) N-M-StrengthAxial Force-Bending (stability) N-M-Stab. Shear (y)Qy Shear (z)Qz*Equivalent Stress in the Web at the FlangeSrCross-Section Shear Factor (y)ShyCross-Section Shear Factor (z)Shz$Cross-Section Elasticity Modulus (y)Wely$Cross-Section Elasticity Modulus (z)WelzMaximum SlendernessLmax!Minimum Buckling Reduction FactorFimin!Lateral Buckling Reduction FactorFiGd.mm.yyhh.mmOpen an AxisVM Model AxisVM ModelsAxisVM Trial VersionPreview PropertiesResult file existsNo result file found Model file Result fileVersionCreatedModifiedSize Look &in: Save &in: File &name:Files of &type:Save as &type:&Help&Save&OpenOpen as &read-onlyPerspective SettingsObservation DistanceWireframe View Rendered View;Zoom in|Performs a zoom in by defining a rectangular region>Zoom out|Performs a zoom out by defining a rectangular regionCFit in window|Scales the view to fit the model in the active windowPanRotate)Displays the model projected to Plane X-Z)Displays the model projected to Plane X-Z)Displays the model projected to Plane X-ZRotation around the X axisRotation around the Y axisRotation around the Z axisModifyNew=Invalid name|You have already defined a perspective named %s.#Delete|Delete perspective named %s?Rendered Model Lights Off Lights On Rendering... Saving ModelAxisVM Model and Results AxisVM Model File Format:AxisVM 7AxisVM 6.0 R10 AxisVM 6.0 R4 AxisVM 6.0 R3 AxisVM 5.0 Axis-3D 4.0 Axis-3D 3.6 Axis-3D 3.5 Axis-3D 3.0Save AxisVM drawing Materials Functions Section Lines PerspectivesPartsCross-Sections Load Groups Load CasesParts Section LinesPerspective Settings MaterialsCross-Sections DimensionsModel InformationCloseModelResultExploring Drive %sExploring drives...%s free%d of %d files%d filesNameSavedNewRename Copy/MoveOpen$Copy|Copying %d files from folder %sTarget folder:Copy result files Move filesInvalid folder)Folder %s does not exists. Create folder? Copy|Copying "%s" from folder %s File name:Copy result file Move file-Copy error|File cannot be copied onto itself.CCannot delete|"%s" is a read-only file therefore cannot be deleted. Delete|Delete %d from folder %s?Delete results only"Delete|Delete "%s" from folder %s?:Invalid name|Folder %s already contains a file named "%s".:Path incomplete|Specify full path of the folder to create.,Drive access error|Drive %s is unaccessible.7New folder|Enter a name for the folder to create in %s.Out of disk space|Drive %s should have %s of free space to complete the copy operation but only %s is available. Make a new selection or change target drive.COverwrite|A file named "%s" already exists in folder %s. Overwrite?-Cannot delete|"%s" is currently being edited.0Cannot overwrite|"%s" is currently being edited.-Cannot rename|"%s" is currently being edited.Enter a new name for "%s". Model Library#File not found|"%s" does not exist..File is read-only|Remove the write protection?5File is read-only|Write protection cannot be removed.Load the file anyway?6Overwrite|A file named "%s" already exists. Overwrite?RFile already exists|Specify a new name before saving a file in an earlier version.2Cannot save file|This file is marked as read-only.5You have modified the model. Results will be cleared.Confirm Save changes?4You have modified the model or the display settings.Model file recovered;An error must have encountered during the previous session.-The model has been reopened at startup as %s. RecoveredAnalysisModel is unchanged.Start the analysis?Invalid filename5File name is too long or contains invalid characters.2Cannot find %s or Acrobat Reader is not installed.pToo many truss/beam or rib elements. This version allows the use of maximum %d truss or %d beam or rib elements!VToo many surface elements. This version allows the use of maximum %d surface elements!RTo many load cases elements. This version allows the use of maximum %d load cases!=This version do not allow the use of truss and beam elements!6This version do not allow the use of surface elements!Method &Incremental &Distribute&Spread by distance &Consecutive&MoveCopy &elements Copy &loadsCopy dimension s&ymbolsNodes to connect&NoneDo&uble selected&AllNdWValue too large|N cannot be greater than %d. Make more copies by repeating the command.N >= 1.Invalid number of copies.AYou cannot specify a distance smaller than the editing tolerance.With DXF &LayerRotationSpread by angle\ah2Value too high|The angle cannot be more than 360°.Zero angle cannot be specified.Mirror&Copy &Multiple&Move&ResizeScaleSelect elements of %sNew part definition Part nameDelete|Delete part named %s?Delete|Delete all parts?)Deleting a part does not delete elements.,Invalid name|A part named %s already exists.Selected/defined parts Auto RefreshEdgeHole%d of %d1 Node%d Nodes1 Truss %d Trusses1 Beam%d Beams1 Rib%d Ribs 1 Membrane %d Membranes1 Plate %d Plates1 Shell %d Shells1 Domain (Membrane)%d Domains (Membranes)1 Domain (Plate)%d Domains(Plates)1 Domain (Shell)%d Domains(Shells) Delete All/Select edges defining the section line named %sNew Section Line Section Name$Delete|Delete section line named %s?+Delete|Delete all section lines and planes?=Invalid name|A section line or plane named %s already exists.Section Lines & PlanesNew Section LineNew Section PlaneNew Section PlaneSection Plane Name%Delete|Delete section plane named %s?5Invalid name|A section plane named %s already exists.Draw Section Plane ContourCalculating intersections...Complete the rectangleEnter a rectangle corner.Generating Rectangles.The command does not work in perspective view. Enter a rectangle side end pointComplete the rectangleEnter a rectangle cornerGenerate Skewed Rectangles!Click a line or a point on a line Click a second point on the lineEnter arc centerpointEnter arc startpointEnter arc endpointEnter first point of circleEnter second point of circleEnter third point of circleEnter arc endpointDivided Triangle DefinitionDistorted triangle|RThe angle at the first vertex of a triangle is %d°. It should be greater than %d°.SThe angle at the second vertex of a triangle is %d°. It should be greater than %d°.RThe angle at the third vertex of a triangle is %d°. It should be greater than %d°.2The use of this finite element is not recommended.Create division anyway?Colinear points Acute angle smaller than minimum#Enter second vertex of the triangleComplete the triangle"Enter first vertex of the triangleGenerating mesh...Divided Quad DefinitionDistorted Quad5Acute angle smaller than minimum at the first vertex.6Acute angle smaller than minimum at the second vertex.5Acute angle smaller than minimum at the third vertex.6Acute angle smaller than minimum at the fourth vertex."Mesh contains distorted triangles.2The use of this finite element is not recommended.6Obtuse angle greater than maximum at the first vertex.7Obtuse angle greater than maximum at the second vertex.6Obtuse angle greater than maximum at the third vertex.7Obtuse angle greater than maximum at the fourth vertex."The mesh contains distorted quads.FQuad side ratio and division numbers would result in a distorted mesh. Acute angle smaller than minimum!Obtuse angle greater than maximumFQuad side ratio and division numbers would result in a distorted mesh. Concave quadEnter first vertexEnter second vertexEnter third vertex Complete Quad-For division lines use depth constraint only.Enter guideline position"Enter first point of the guideline$Enter another point of the guideline>Ctrl+click places a new guideline parallel to the previous one"Drag guideline to its new position)For guidelines use depth constraint only.Select entities to translateSelect nodes to connectMaking copies...Making a copy...Translation...Enter translation vectorEnter translation base pointSelect entities to rotateEnter rotation center pointEnter rotation arc start pointComplete rotation arcSelect entities to mirror Mirroring...Generating image...(Enter a second point of the mirror plane!Enter a point of the mirror planeSelect nodes to scale Rescaling...Enter scale center pointEnter scale reference point,Enter reference point in its scaled positionSelect lines to divideTruss %dBeam %dRib %dLine %d. (Edge)Line %dLine %d%d selected truss(es)%d selected beam(s)%d selected rib(s)%d selected line(s) (edges).%d selected lines (on undefined surface edges)%d selected linesSelect lines to intersect)Select edges to identify surface elements Find SurfacesNew elements found:Searching for surfaces.../Select nodes you want to refine the mesh aroundRefine Mesh Around NodesInvalid selection!Adjacent nodes cannot be selected,No proper nodes selected for mesh refinement/Select lines you want to refine the mesh aroundRefine Mesh Along Edges5Selection does not allow mesh refinement along edges ,No proper lines selected for mesh refinementChecking triangles to divide...Checking quads to divide...+Select surface elements for mesh refinement6Select surface elements you want to refine the mesh inGenerate Uniform MeshMesh refinement"Perpendicular constraint undefinedLinear Analysis of %sNonlinear Analysis of %sVibration Analysis of %sVibration Analysis of %sBuckling Analysis of %sError in AnalysisSave model before analysisModelNumber of EquationsEquations MemoryEstimated Memory RequirementModel VerificationAnalysisResult File GenerationCancelAnalysis of %s completed.DetailsResult File Size: %s.Solution ErrorInternal ErrorInvalid rotation matrix.)Invalid coordinate transformation matrix.%Singular metric interpolation matrix.'System matrix is not positive definite.%Ill conditioning estimator too large.Singular Jacobian matrix.9Model contains very distorted elements. Improve the mesh.0Excessive element distortion during deformation.3Excessive distortion of Beam %d during deformation.4Excessive distortion of Truss %d during deformation.2Excessive distortion of Rib %d during deformation.>Excessive distortion of surface element %d during deformation.(Too large rotation increment at node %d.=Specify greater number of increments to run this calculation.%Invalid DOF for displacement control.$Divergence in the current iteration.-Probable divergence in the current iteration.%No convergence in maximum iterations.!The model contains singularities.CCheck nodal DOF, support conditions, and beam end release settings.źNot enough mass degrees of freedom to obtain the requested number of eigenvalues. Maximum number of model eigenvalues is %d. Increase mass DOFs or decrease number of requested eigenvalues./No eigenvalue found within the tolerance limit.FThere are %d missing eigenvalues less than upper bound of those found."No axial forces to cause buckling.Invalid Topology=Calculation would require more virtual memory than available.:%s of virtual memory is necessary to run this calculation.File I/O error.)Node %d has no stiffness in %s direction.&Equations would require more than 2GB.AIt exceeds the maximum memory size available for the application.3Divide the model into smaller parts or simplify it./Singular Jacobian matrix at surface element %d. Input ErrorsVirtual Memory Too LownMake sure that you have set the maximum paging file size larger than the memory required for this calculation.DThis value can be set in the dialog Control Panel/System/Perfomance.CCheck if the model has proper translational or rotational supports. Model contains unbalanced loads.WUsually it is the result of a fixed nodal degree of freedom in the direction of a load.Check nodal degrees of freedom.:You can find load values in the table of unbalanced loads.!Creating critical combinations...8Cannot run nonlinear analysis for critical combinations.;No loads groups defined for creating critical combinations.$Cannot create critical combinations.)Check if you grouped load cases properly.qTo create a critical combination first run a linear analysis then a nonlinear one using the actual reinforcement.Total physical memoryAvailable physical memory Range error.Value %d cannot be stored. Interval:[-30,223].Invalid panel index-%d is an invalid panel index in the Registry.Default%d active part(s)Nonlinear Static AnalysisSolution ControlCaseForce DisplacementNode: Direction:Number of increments:Maximum Iterations:'Update stiffnesses each n-th iterationsAStifnesses must be updated at least twice in each increment (%s).Convergence Criteria DisplacementWork.No load case available for nonlinear analysis. Load Factor:Maximal Displacement:Include geometric nonlinearity7Save results for use in vibration and buckling analysisNode index not found.$Select the node for analysis control‡Nonlinear analysis of surface structures can be performed only if the model contains a nonlinear truss, spring, support or gap element.'Use actual reinforcement in calculationStore last increment onlyYesNoExitHelpAllNN has a maximum of 200N must be greater than zeroCreating Surfaces#N has a maximum of 200 on each side(N must be greater than zero on each sideAdd8Sets selection mode to add entities to the selection setRemove=Sets selection mode to remove entities from the selection setInvert4Sets selection mode to invert status of the entitiesMethodSets method of selectionAllEApplies the selection operation to all entity types set in the filterRestoreRestores the previous selectionFilter&Sets the entities that can be selectedAccept the selection setCancel selection5Applies the selection operation to elements of parts.Selection of partsFilterPointsLinesEdgeLineSurfacesSurfaceDomainsHolesSupportsNodalLinearSurface ReferencesProperty &Filtering...Checking nodes...Checking lines...Checking surfaces...Checking supports...Checking loads...Checking nodal masses...Nodes deleted:Lines deleted:Surfaces deleted:Number of unattached nodes::One or more selected lines are shorter than the set value. These lines will not be divided. Divide LineMethod By &Ratio By &LengthInto &N equal parts&Uniform by lengthTThis point is the same as the end point (within the tolerance). Division is skipped.#Division ratio must be less than 1.8This value is greater than the length of selected lines.OThe maximum number of division is 200. For further division repeat the command.adNVThis point is the same as the start point (within the tolerance). Division is skipped.2The line should be dived at least in two segments.Geometry Check Importing %s ToleranceGeometry Check Tolerance Select unattached nodes or lines&File&Open...&Save... Save &As...1Saves the model with a different name or location&Model Library...BDisplays file information, preview, and allows file administrationMa&terial Library...5Opens material library to select and define materialsE&xitCCloses this program after prompting to save any unsaved information&EditUndoRedoUndo %sRedo %s &Settings&Preferences...'Sets global preferences for the program&Units and Formats...;Sets the units and number formats to be used by the program&View&Fit in Window,Scales the model to fit in the active window &Perspective,Sets a perspective view in the active windowSetting Perspective View... &Front View>Displays the model projected to Plane X-Z in the active window &Side View>Displays the model projected to Plane Y-Z in the active window &Top View>Displays the model projected to Plane X-Y in the active window&Zoom inDMagnifies the display within a rectangle to fit in the active windowZoom out>Reduces the active window display by scaling it to a rectangle&Window&Information WindowsShows/hides information windows&Status7Displays basic information on model and window settings &CoordinatesBDisplays current cursor position and allows editing of coordinates Color &LegendOTable of current colors and value limits used when displaying result componentsSplit &Horizontally%Splits the active window horizontallySplit &Vertically#Splits the active window vertically &Close WindowCloses the active windowHel&p Line ElementsSurface Elements Nodal SupportDefines/modifies nodal supports Line SupportDefines/modifies line supportsSurface Support!Defines/modifies surface supportsUniform Refinement?Refines mesh evenly based on a maximum finite element side size(Generates or refines a mesh around nodes'Generates or refines a mesh along edgesRefinement by BisectionAuto RefinementGenerates mesh for polygonsLinear Static AnalysisNonlinear Static AnalysisVibration AnalysisVibration AnalysisBuckling AnalysisElementsGeometry Buckling R.C. Design VibrationStaticLoads Steel DesignAxisVMError%No cross-section defined in the model No material defined in the model;Neither cross-section nor material is defined in the model.No reference defined.*Neither material nor reference is defined.Select the elements Envelope Min Envelope MaxEnvelope Min,Max Critical Min. Critical Max.Critical Min,Max. Critical Min. Critical Max.Critical Min,Max. Displacements Rotations Axial Forces Shear ForcesTorsional MomentsFlexural MomentsPrincipal ForcesPrincipal DirectionsPrincipal MomentsDiagram Section LineMembrane Forces Plate MomentsPlate Shear ForcesR. Design Membrance ForcesR. Design MomentIsoline IsosurfaceIntensity variationNoneInvalid setting=No section lines or planes defined. This setting is inactive.DAll section lines and planes are disabled. This setting is inactive. &Export... Saves the model in other formats &Import...Reads data having other formatsC&ross-Section Library...AOpens cross-section libraries to select and define cross-sectionsPage &Header...(Sets the page header of printing reportsPrint Set&up...Selects and configures printersPrint...5Sends the model view to printer or to a graphics file"Sends printer files to the printer&Copy4Copies drawing in the active window to the ClipboardCu&t&Paste&Symbols(Sets display options for graphic symbols&Labels'Sets display options for element labels S&witches!Sets display options for entities&Edit &Contents Help Contents&IndexFinds keywords in Help Help &On Help%Provides instructions to use the Help &About...SpringDefines/modifies springsGap Gap ElementsDefines/modifies gap elementsLinkDefines/modifies link elements No envelopeCNo load case or load combination selected for envelope calculation.QSet load cases or load combinations in the Result Display Options dialogue windowLoad Cases & Load Groups>Creates, deletes, renames, modifies load cases and load groupsLoad Combinations,Creates, deletes, modifies load combinations &Delete...*Allows deletion based on current selection Select &All4Selects all elements matching the filtering criteriaLinear AnalysisNonlinear AnalysisMin, Max ValuesResult Display ParametersRefresh2Click a node to pick up the result component from.%Press TAB to select the next element.&Options&Grid && Cursor... &Editing... &Views...&Design Codes...&Gravitation... AnimationDiagram DisplayVibration AnalysisBuckling AnalysisReinforcement ParametersActual column reinforcementColumn ReinforcementBeam Reinforcement Calculation4Import Error|Files cannot be imported in result viewActual ReinforcementError in Selection,Selected elements cannot be analyzed as one.8Check their materials, cross-sections and local systems.+Select one or more connecting beams or ribsAxisVM Home &Page;Visits AxisVM Home Page using your default Internet browser AxisVM Update0Starts the download of the latest AxisVM release&Guidelines Setup$Moves, creates or deletes guidelinesAuto Intersection:Selected columns have different lengths or cross-sections.QSelect elements of same properties by setting the filter on the selection toolbarCIf you continue specify a column cross-section and a column length.aThe reinforcement check will be calculated according to the internal forces of selected elements. Continue?(Select columns for reinforcement design ReinforcedSave active window as &RTF file &Wireframe&Hidden line removal &RenderedWireframe while &dragging Joint designDesign of bolted joints%Initialization error|Error code: %.2d Joint designAdd drawing to GalleryAdd drawing to Gallery/A model named %s has been found in this folder.Load that model now?Perspective settingsRSelect nonvertical line elements and one of their end nodes to analyse connection.Display ParametersParts... Symbols... View UndoComplete SelectionModify Line Element...Modify Surface Element...Modify Support...Modify Load...Modify Nodal Coordinates... Modify DOF...Modify Reference...Modify region...Modify Link...Reference already existsEnter reference point)This reference point already exists. (%d),Enter the base point of the reference vector,Enter the end point of the reference vector =A reference vector of the same direction already exists. (%d)Invalid reference7Reference vector base point and end point are the same.#Enter a point of the reference axis)Enter another point of the reference axis;A reference axis of the same direction already exists. (%d)(The two axis points entered are the same$Enter a point of the reference plane+Enter a second point of the reference plane*Enter a third point of the reference plane/A parallel reference plane already exists. (%d)&The three points entered are colinear.%Enter a point of the section plane %s,Enter a second point of the section plane %s+Enter a third point of the section plane %sSurface without PropertiesBThe surface element you have chosen has no properties to pick up. ]The local x reference of this surface is invalid for some of the selected surface elements . Invalid reference\The local z reference of this surface is invalid for some of the selected surface elements. >Thickness of this surface is smaller than the minimum allowed.DThis surface has an unallowed negative thickness. Correct the value.Click a surface elementClick a local x referenceMThis local x reference is invalid for some of the selected surface elements. Click a local z referenceMThis local z reference is invalid for some of the selected surface elements. Select surfacesSelection cannot be overwritten`Selection consists of surfaces with rigid bodies on sides. These elements cannot be overwritten.Surface ElementsDomains Domain %dDom. %dDomain %d (membrane)Domain %d (plate)Domain %d (shell)Hole %d Membrane %dPlate %dShell %d Surface %dNew Surface ElementYSelection contains a surface without properties but a common x reference cannot be found.YSelection contains a surface without properties but a common z reference cannot be found.!Surface element cannot be defined)A mesh line has no properties to pick up.%An edge has no properties to pick up.%An edge has no properties to pick up.+Gap element properties cannot be picked up..Spring element properties cannot be picked up.,Link element properties cannot be picked up.Properties cannot be picked up]The local z reference of this line element is invalid for some of the selected line elements.Click a line elementClick a local z referenceIThis local z reference is invalid for some of the selected line elements.,Select line elements and connecting surfacesESelection consists of rigid elements only, that cannot be overwrittenDSelection consists of link elements only, that cannot be overwritten Line ElementsVSelection contains a line without properties but a common z reference cannot be found.Cannot define line elementClick a node or a midside node!Select nodes and/or midside nodesNodal Degrees of FreedomNode %dMidside Point of Rib %dMidside Point of Edge&A spring must have a nonzero stiffness%Springs must have a nonzero stiffness&Springs must have a nonzero stiffness.H%d springs are selected. %s of them would not have stiffness parameters.OThe local z reference of this spring is invalid for some of the selected lines.OThe local x reference of this spring is invalid for some of the selected lines.NThe x reference node of this spring is invalid for some of the selected lines.NThe z reference node of this spring is invalid for some of the selected lines.Click a springClick a local z referenceIThis local x reference is invalid for some of the selected line elements.Click a local z referenceJThis local z reference is invalid for some of the selected line elements. ,Click an element to pick up its local systemClick an x reference nodeClick a z reference nodeSprings Spring %dGapsGap %dClick a gap element"Select domains or their boundariesSelect hole boundaries!Click a surface element or domainInvalid domain selection8No domain can be defined based on the current selection.Check the following criteriaDDomains will be created from the contour of lines on the same plane.7The contour of selected lines must be a closed polygon.GLines of an automatic mesh are not allowed to define domain boundaries.>Beams and trusses are not allowed to define domain boundaries.JThe contour of selected lines cannot intersect existing domain boundaries.*Select domains to apply automatic meshing.Meshing Error #%dInvalid hole selection5No hole can be defined based on the current selectionTThe local x reference of this surface is invalid for some of the selected domains . SThe local z reference of this surface is invalid for some of the selected domains. Meshing ErrorMCheck the model at the selected nodes and lines or try a different mesh size.eSome of the intervals between nodes or lines proved to be too small. This may indicate design errors.DMesh generation failed at the selected points with these parameters.@Check domain boundaries and inner lines near the selected nodes.7Domain %d includes isolated nodes on elements or edges."Delete these nodes before meshing.7Meshing error near independent points inside Domain %d.hDomain %d contains an indivisible element or edge longer than three times the average mesh element size.%d element(s), %d domain(s)Cannot define node to node link elements on consecutive lines.^For certain elements no master nodes were selected. Link element positions will be set to 1/2.Click a link element,A link element must have a nonzero stiffness#Links must have a nonzero stiffness,Link elements must have a nonzero stiffness.N%d link elements are selected. %s of them would not have stiffness parameters.MThe local z reference of this link is invalid for some of the selected lines.MThe local x reference of this link is invalid for some of the selected lines.LThe x reference node of this link is invalid for some of the selected lines.LThe z reference node of this link is invalid for some of the selected lines. Link elementsLink %dN-NL-LS-SdSelect link elements and/or lines forming a quadrangle to define link elements between edges or ribsSelect master midside nodes9Some parts of this selection do not define link elements.4Change local system of the link element by geometry?2Change local system of the link element to global?%Change local system of link elements?Invalid selection7Cannot define link element from certain selected lines._If selection remains the same link elements will be defined from the proper line elements only.Change selection?FSelection is incomplete. Cannot set master node for all link elements.2Select elements to perform design calculations forColor Legend SetupOther settings...LevelsLimitsMin, Max of ModelMin, Max of PartsAbsolute Max. of ModelAbsolute Max. of PartsCustomAuto Interpolate Refresh All)Range values must be in descending order. Calcula&te... Saving SeriesEnter a name for this series.Name6Overwrite|A series named %s already exists. Overwrite? Save As... Save &As...Delete & Rename Series...EXPDecimalsNumber of decimals to displayUnits and Formats Units Scheme Save As...Structure size Thickness Beam LengthSurfaceGeometryDistanceAngle StiffnessRotational stiffnessTranslational stiffnessLine translational stiffnessLine rotational stiffnessSurface stiffness Translational Rotational Cross-sectionCross-section sizeCross-section areaLengthAreaVolumeInertiaLoadsForceMoment Line force Surface force Line Moment TemperatureTemperature VariationMass Per Length MiscellaneousTimeGravitation (g)Material Properties!Young’s Modulus of Elasticity (E)"Thermal Expansion Coefficient (\a) Stress (\s)MassMass Density (\r)Results DisplacementRotationForceMomentLine support internal forceLine support internal momentSurface support internal forceStress ReinforcementCracking FrequencyCircular FrequencyPeriodSpeedStrength Gap OpeningMode Shape DisplacementMode Shape RotationInfluence line ordinateWarping constant Static momentSteel design check componentsRebar diameterRebar distancePoisson’s RatioIntensity variationInfluence line forceInfluence line momentAggregate size Safety FactorLoad combination factorLimiting StrainBuckling factorReinforcement area Steel DesignGap stiffness adjustment ratioInterface locationSeismic equivalence coefficient Beta FactorLoad position ratio Eccentricity*Compressive strength reduction factor (\a)Creeping factor (\f_ _t)Set current settings as default0You have already defined a unit scheme named %s. Scheme NameNew Units SchemeDelete units scheme %s?CustomUnitDec.Geometry Cross-sectionElement Properties R.C. Design VibrationStatic DimensioningSize DimensionAngle DimensionDimension symbol graphics sizeNodal Degrees of Freedom Free node Fixed nodeTruss girder in Plane X-YTruss girder in Plane X-ZTruss girder in Plane Y-Z Space trussFrame in plane X-YFrame in plane X-ZFrame in plane Y-ZGrillage in plane X-YGrillage in plane X-ZGrillage in plane Y-ZMembrane in plane X-YMembrane in plane X-ZMembrane in plane Y-ZPlate in plane X-YPlate in plane X-ZPlate in plane Y-ZX-Y symmetry planeX-Z symmetry planeY-Z symmetry planeX-Y antimetry planeX-Z antimetry planeY-Z antimetry planeUnion Overwritee_Xe_Ye_Z\q_X\q_Y\q_ZFree Constrained*Prescribed DisplacementModify Degrees of FreedomChoose a ColorMore &Colors...#Selects entities within a rectangle*Selects entities within a skewed rectangle Selects entities within a sectorSelects entities within a ringLoads cannot be zero)To remove selected nodal load, delete it.,To remove selected nodal loads, delete them."Selected nodal load would be zero.6%d nodal loads are selected. %d of them would be zero.To remove loads delete them. Zero LoadClick a node with loads"Press TAB to select the next load.Select nodes to apply loads Nodal LoadsNodal Loads on Node %dPThis reference is on one of the selected nodes and could not define a direction.(Select beams to apply concentrated loads'Select beams to apply distributed loadsConcentrated Loads on BeamsConcentrated Loads on Beam %dConcentrated Loads on Rib %d#Distributed Loads on Beams and RibsDistributed Loads on Beam %dDistributed Loads on Rib %d$Click a beam with concentrated loads*Click a beam or rib with distributed loads4To remove the selected concentrated load, delete it.7To remove the selected concentrated loads, delete them.3To remove the selected distributed load, delete it.5To remove the selected distrbuted loads, delete them./To remove the selected thermal load, delete it.2To remove the selected thermal loads, delete them.,To remove the selected edge load, delete it./To remove the selected edge loads, delete them.5Select trusses, beams and ribs to apply thermal loads