{"id":381315,"date":"2024-09-02T08:40:38","date_gmt":"2024-09-02T08:40:38","guid":{"rendered":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/reinf265-as-steel-wire-reinfocements-for-spiral-arrangements-apdl\/"},"modified":"2024-09-02T08:40:38","modified_gmt":"2024-09-02T08:40:38","slug":"reinf265-as-steel-wire-reinfocements-for-spiral-arrangements-apdl","status":"publish","type":"topic","link":"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/reinf265-as-steel-wire-reinfocements-for-spiral-arrangements-apdl\/","title":{"rendered":"Reinf265 as steel wire reinfocements for spiral arrangements APDL"},"content":{"rendered":"<p>&lt;p&gt;Hi everyone I am using Reinf265 with solid 185 as steel wire reinfocements &nbsp;for spiral arrangements of wire along tube.Its a hydraulic tube consists of rubber as base material and&nbsp; 4 layers of steel wire as reinforcements.My model consists of three types of&nbsp; rubber material and steel wire reinforcements.<strong>Please comment is smeared reinforcing approach is okay to use,or discret approach should be used<\/strong>&nbsp; I have a problem material 2 in my model represnts as steel and material 1 represents base rubber material.In reinforcing section material 2 is alloted to reinforcement with other properties like area,spacing etc but when i tried to check the material of reinforcing it is still showing base material 1,is it normal or it should represents material2.please check my model.I am thinking reinforcement is not applied correctly. First screenshot represnt model with different materials.2nd represents model + reinforcing and&nbsp; 3rd&nbsp; represnts only reinforcing material (for my query material should be 1+ 2 or 2 only)&nbsp;&nbsp; .<img decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/09\/02-09-2024-1725266340-mceclip0.jpg\" \/>&lt;\/p&gt;&lt;p&gt;<img decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/09\/02-09-2024-1725266393-mceclip1.jpg\" \/>&lt;\/p&gt;&lt;p&gt;<img decoding=\"async\" src=\"https:\/\/innovationspace.ansys.com\/forum\/wp-content\/uploads\/sites\/2\/2024\/09\/02-09-2024-1725266398-mceclip2.jpg\" \/>fini&lt;br&gt;\/cle&lt;br&gt;&nbsp;&lt;br&gt;\/sys,del file*.png&lt;br&gt;&nbsp;&lt;br&gt;\/vie,1,1,1,1&lt;br&gt;\/vup,1,z&lt;\/p&gt;&lt;p&gt;C********************************************************&lt;br&gt;C*** PARAMETERS&lt;br&gt;C********************************************************&lt;br&gt;pi=acos(-1)&lt;\/p&gt;&lt;p&gt;r1=12.5 ! CYLINDER INNER RADIUS&lt;br&gt;r2=14.40 &nbsp;! Rubber Layer 1&nbsp;&lt;br&gt;r3=14.60 ! Fabric Layer&lt;br&gt;r4=14.75 ! Tela Layer&lt;br&gt;r5=15.35 ! Steel Reinforcement Layer 1&lt;br&gt;r6=15.50 ! Rubber Layer 2&lt;br&gt;r7=16.10 ! Steel Reinforcement Layer 2&lt;br&gt;r8=16.25 ! Rubber Layer 3&lt;br&gt;r9=16.85 ! Steel Reinforcement Layer 3&lt;br&gt;r10=17.0 ! Rubber Layer 4&lt;br&gt;r11=17.60 ! Steel Reinforcement Layer 4&lt;br&gt;r12=19.2 ! CYLINDER OUTER RADIUS&lt;br&gt;l=180 ! CYLINDER LENGTH&lt;br&gt;r_reinf=0.3 &nbsp;! REINFORCING FIBER RADIUS&lt;br&gt;a=pi*r_reinf**2 &nbsp;! REINFORCING FIBER CROSS SECTION AREA&lt;br&gt;facenum=3 &nbsp;! FACE NUMBER FOR &#8220;ELEF&#8221; REINF SECTION PARAMETER&lt;br&gt;s=0.275 &nbsp;! REINFORCEMENT SPACING&lt;br&gt;thta=54.04 &nbsp;! MAGNITUDE OF REINFORCING FIBER ORIENTATION ANGLE&lt;br&gt;thta1=54.08 &nbsp;! MAGNITUDE OF REINFORCING FIBER ORIENTATION ANGLE&lt;br&gt;thta2=54.90 &nbsp;! MAGNITUDE OF REINFORCING FIBER ORIENTATION ANGLE&lt;br&gt;thta3=54.103 ! MAGNITUDE OF REINFORCING FIBER ORIENTATION ANGLE&lt;\/p&gt;&lt;p&gt;E_base=3 ! BASE ELEMENT FOR REINFORCEMENTS (~RUBBER)&lt;br&gt;nu_base=0.4 ! BASE ELEMENET POISSON&#8217;S&lt;br&gt;&nbsp;&lt;br&gt;E_reinf=0.21e6 ! REINF ELASTIC MODULUS&lt;br&gt;nu_reinf=0.30 ! REINF POISSON&#8217;S&lt;br&gt;\/title,R_fiber=%r_reinf%, S_fiber=%s%, E_fiber=%E_reinf%&lt;\/p&gt;&lt;p&gt;C********************************************************&lt;br&gt;C*** GEOMETRY &amp; BASE ELEMENT MESH&lt;br&gt;C********************************************************&lt;br&gt;wpcs,-1,0 &nbsp;! CYLINDRICAL ELEMENT COORDINATE SYSTEM&lt;br&gt;cswp,11,1&lt;\/p&gt;&lt;p&gt;\/prep7 &nbsp;! GEOMETRY (CREATING SIX 60 DEG SECTORS)&lt;br&gt;cyli,r1,r2,0,l,0,90 &nbsp;! Layer 1: Rubber&lt;br&gt;cyli,r2,r3,0,l,0,90 &nbsp;! Layer 2: Fabric&lt;br&gt;cyli,r3,r4,0,l,0,90 &nbsp;! Layer 3: Tela&lt;br&gt;cyli,r4,r5,0,l,0,90 &nbsp;! Layer 4: Steel Reinforcement Layer 1&lt;br&gt;cyli,r5,r6,0,l,0,90 &nbsp;! Layer 5: Rubber&lt;br&gt;cyli,r6,r7,0,l,0,90 &nbsp;! Layer 6: Steel Reinforcement Layer 2&lt;br&gt;cyli,r7,r8,0,l,0,90 &nbsp;! Layer 7: Rubber&lt;br&gt;cyli,r8,r9,0,l,0,90 &nbsp;! Layer 8: Steel Reinforcement Layer 3&lt;br&gt;cyli,r9,r10,0,l,0,90 &nbsp;! Layer 9: Rubber&lt;br&gt;cyli,r10,r11,0,l,0,90 &nbsp;! Layer 10: Steel Reinforcement Layer 4&lt;br&gt;cyli,r11,r12,0,l,0,90 &nbsp;! Layer 11: Rubber&lt;br&gt;! Add Steel Cap at the bottom end&lt;\/p&gt;&lt;p&gt;numm,kp ! MERGE COINCIDENT KEYPOINTS&lt;br&gt;vatt,1,1,1,11 ! ASSIGN ATTRIBUTE NUMBERS (MAT, REAL, TYPE, ESYS)&lt;br&gt;&nbsp;&lt;br&gt;et,1,185,,,1 ! LAYERED SOLID185 ELEMENT TYPE&lt;br&gt;mp,ex,1,E_base ! ELASTIC MODULUS&lt;br&gt;mp,nuxy,1,nu_base ! POISSON&#8217;S&lt;br&gt;vmes,3,10 ! MESH VOLUME&lt;br&gt;vsel, all &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Clear selection&lt;\/p&gt;&lt;p&gt;! Define the hyperelastic material model for the inner rubber&lt;br&gt;tb, hyper, 3, 1, 6, mooney &nbsp;! Mooney-Rivlin hyperelastic model, material 1, 6 constants&lt;br&gt;tbdata, 1, -58.285, 69.245, 45.908, -148.61, 150.8, 0.2145 &nbsp;! Mooney-Rivlin constants&lt;\/p&gt;&lt;p&gt;! Define the hyperelastic material model for the inner rubber using 3 Mooney-Rivlin parameters&lt;\/p&gt;&lt;p&gt;tb, hyper, 4, 1, 4, mooney &nbsp;! Mooney-Rivlin hyperelastic model, material 3, 4 constants&lt;br&gt;tbdata, 1, -10.343, 17.456, 4.504, 0.332 &nbsp;! Mooney-Rivlin constants C10, C01, C11, D1&lt;\/p&gt;&lt;p&gt;&lt;br&gt;! Select and mesh volumes for Material 1&lt;br&gt;vsel, s, cent, x, r1, r3 &nbsp;! Select volumes from r1 to r3&lt;br&gt;vatt, 3, 1, 1, 11 &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Assign Material 1&lt;br&gt;vmesh, 1,2 &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; ! Mesh only the selected volumes (Material 1)&lt;br&gt;vsel, all &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Clear selection&lt;\/p&gt;&lt;p&gt;! Select and mesh volumes for Material 3&lt;br&gt;!vsel, s, cent, x, r3, r11 &nbsp;! Select volumes from r3 to r11&lt;br&gt;!vatt, 3, 1, 1, 11 &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Assign Material 3&lt;br&gt;!vmesh, 2,10 &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; ! Mesh only the selected volumes (Material 3)&lt;br&gt;!vsel, all &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Clear selection&lt;\/p&gt;&lt;p&gt;! Select and mesh volumes for Material 4&lt;br&gt;vsel, s, cent, x, r11, r12 &nbsp;! Select volumes from r11 to r12&lt;br&gt;vatt, 4, 1, 1, 11 &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Assign Material 4&lt;br&gt;vmesh, 11 &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; ! Mesh only the selected volumes (Material 4)&lt;br&gt;vsel, all &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp;! Clear selection&lt;br&gt;! Define the geometry of the steel cap&lt;br&gt;! Assume that the steel cap has an inner radius of r1, outer radius of r2, and height of -0.01 m (or -10 mm)&lt;br&gt;cyli,0,r12,-10,0,0,90 &nbsp;! Steel Cap at bottom end (0 to -10 mm)&lt;\/p&gt;&lt;p&gt;! Assign the attribute to the newly created volume&lt;br&gt;vatt,2,2,1,1 &nbsp;! Assign material 2 to the volume (volumes are indexed; you might need to adjust if your volume index is different)&lt;br&gt;vsel, s, cent, x, 0, r12,z&lt;br&gt;! Set the element type for the steel cap&lt;br&gt;et,1,185 &nbsp;! Use a solid element type; adjust if needed based on your model&lt;\/p&gt;&lt;p&gt;! Mesh the volume with simple mesh&lt;br&gt;! Here we use free meshing; adjust the mesh size as needed&lt;br&gt;vmesh,12&lt;br&gt;C********************************************************&lt;br&gt;C*** REORIENT BASE ELEMENTS&lt;br&gt;C********************************************************&lt;br&gt;eorient,lysl,posz &nbsp;! ORIENT ELEMENTS SO THAT FACE 1 IS PARALLEL TO +Z AXIS&lt;\/p&gt;&lt;p&gt;C********************************************************&lt;br&gt;C*** MATERIAL PROPERTIES FOR REINFORCEMENT&lt;br&gt;C********************************************************&lt;br&gt;mp,ex,2,E_reinf &nbsp;! Elastic modulus for reinforcement material&lt;br&gt;mp,nuxy,2,nu_reinf &nbsp;! Poisson&#8217;s ratio for reinforcement material&lt;\/p&gt;&lt;p&gt;C********************************************************&lt;br&gt;C*** DEFINE VOLUME REINFORCEMENT SECTIONS&lt;br&gt;C********************************************************&lt;br&gt;sect,2,reinf,smear &nbsp;! Reinforcement Section 1 (between r4 and r5)&lt;br&gt;secd,2,A,s,,thta,elef,facenum,0&lt;br&gt;seccontrol,0,0,0 &nbsp;! Remove base material in domain occupied by reinforcing&lt;\/p&gt;&lt;p&gt;sect,3,reinf,smear &nbsp;! Reinforcement Section 2 (between r6 and r7)&lt;br&gt;secd,2,A,s,,-thta1,elef,facenum,0&lt;br&gt;seccontrol,0,0,0 ! Remove base material in domain occupied by reinforcing&lt;\/p&gt;&lt;p&gt;sect,4,reinf,smear &nbsp;! Reinforcement Section 3 (between r8 and r9)&lt;br&gt;secd,2,A,s,,thta2,elef,facenum,0&lt;br&gt;seccontrol,0,0,0 ! Remove base material in domain occupied by reinforcing&lt;\/p&gt;&lt;p&gt;sect,5,reinf,smear &nbsp;! Reinforcement Section 4 (between r10 and r11)&lt;br&gt;secd,2,A,s,,-thta3,elef,facenum,0&lt;br&gt;seccontrol,0,0,0 &nbsp;! Remove base material in domain occupied by reinforcing&lt;\/p&gt;&lt;p&gt;C********************************************************&lt;br&gt;C*** APPLYING REINFORCEMENT LAYERS&lt;br&gt;C********************************************************&lt;br&gt;csys,11 &nbsp;! Switch to cylindrical coordinate system (CSYS 11)&lt;\/p&gt;&lt;p&gt;! Layer 1: Apply reinforcement between r4 and r5&lt;\/p&gt;&lt;p&gt;nsel,s,loc,x,14.75,15.35 &nbsp;! Select nodes between r4 and r5 based on x-coordinate&lt;br&gt;nsel,r,loc,z,0,l&nbsp;&lt;br&gt;esln,s &nbsp;! Select elements connected to selected nodes&lt;br&gt;nsle,r &nbsp; ! Ensure all nodes in selected elements are within the specified range&lt;br&gt;secn,2 &nbsp;! Apply first reinforcement section&lt;br&gt;ereinf &nbsp;! Generate reinforcement elements for Layer 1&lt;\/p&gt;&lt;p&gt;alls &nbsp;! Clear selections before moving to the next layer&lt;\/p&gt;&lt;p&gt;&lt;br&gt;! Layer 2: Apply reinforcement between r6 and r7&lt;br&gt;nsel,s,loc,x,15.50,16.10 &nbsp;! Select nodes between r6 and r7&lt;br&gt;nsel,r,loc,z,0,l&nbsp;&lt;br&gt;esln,s &nbsp;! Select elements connected to selected nodes&lt;br&gt;nsle,r &nbsp;! Ensure all nodes in selected elements are within the specified range&lt;br&gt;secn,3 &nbsp;! Apply second reinforcement section&lt;br&gt;ereinf &nbsp;! Generate reinforcement elements for Layer 2&lt;\/p&gt;&lt;p&gt;alls &nbsp;! Clear selections before moving to the next layer&lt;\/p&gt;&lt;p&gt;! Layer 3: Apply reinforcement between r8 and r9&lt;br&gt;nsel,s,loc,x,16.25,16.85 &nbsp;! Select nodes between r8 and r9&lt;br&gt;nsel,r,loc,z,0,l&nbsp;&lt;br&gt;esln,s &nbsp;! Select elements connected to selected nodes&lt;br&gt;nsle,r &nbsp;! Ensure all nodes in selected elements are within the specified range&lt;br&gt;secn,4 &nbsp;! Apply third reinforcement section&lt;br&gt;ereinf &nbsp;! Generate reinforcement elements for Layer 3&lt;\/p&gt;&lt;p&gt;alls &nbsp;! Clear selections before moving to the next layer&lt;\/p&gt;&lt;p&gt;! Layer 4: Apply reinforcement between r10 and r11&lt;br&gt;nsel,s,loc,x,17.0,17.60 &nbsp;! Select nodes between r10 and r11&lt;br&gt;nsel,r,loc,z,0,l&lt;br&gt;esln,s &nbsp;! Select elements connected to selected nodes&lt;br&gt;nsle,r &nbsp;! Ensure all nodes in selected elements are within the specified range&lt;br&gt;secn,5 &nbsp;! Apply fourth reinforcement section&lt;br&gt;ereinf &nbsp;! Generate reinforcement elements for Layer 4&lt;\/p&gt;&lt;p&gt;alls &nbsp;! Clear all selections after the process&lt;br&gt;csys,0 &nbsp;! Return to global coordinate system (CSYS)&lt;br&gt;&nbsp;&lt;br&gt;C********************************************************&lt;br&gt;C*** MAKE BASE ELEMENT HOMOGENEOUS, PLOT ELEMENTS&lt;br&gt;C********************************************************&lt;br&gt;et,1,185 &nbsp;! SET BASE ELEMENT TO HOMOGENEOUS OPTION&lt;\/p&gt;&lt;p&gt;esel,s,type,,1 &nbsp;! MAKE BASE ELEMENTS TRANSLUCENT&lt;br&gt;\/trlcy,elem,0.9&lt;br&gt;alls&lt;br&gt;\/psy,layr,-1 &nbsp;! DISPLAY LAYERS (REINFORCEMENT)&lt;br&gt;\/esh,1&lt;br&gt;\/dev,vect,0 &nbsp;! RASTER FILL DISPLAY&lt;br&gt;eplo &nbsp;! PLOT ELEMENTS&lt;br&gt;\/sho,png $eplo $\/sho,close $\/wait,2&lt;\/p&gt;&lt;p&gt;esel,s,type,,2 &nbsp;! SELECT REINFORCING ELEMENTS&lt;br&gt;\/dev,vect,1 &nbsp;! WIRE FRAME DISPLAY&lt;br&gt;eplo &nbsp;! PLOT ELEMENTS&lt;br&gt;\/sho,png,,1 $eplo $\/sho,close $\/wait,2&lt;\/p&gt;&lt;p&gt;\/dev,vect,0 &nbsp;! REVERT TO RASTER FILL&lt;br&gt;esel,s,type,,1 &nbsp;! MAKE BASE ELEMENTS OPAQUE&lt;br&gt;\/trlcy,elem,0&lt;br&gt;alls&lt;br&gt;! Define boundary conditions and apply pressure loads&lt;\/p&gt;&lt;p&gt;\/solu&lt;\/p&gt;&lt;p&gt;! Fix the base of the tube along the Z-axis&lt;br&gt;!nsel,s,loc,z,l ! Select nodes at Z = 0 (base)&lt;br&gt;!d,all,uz,0 &nbsp; &nbsp; ! Fix all degrees of freedom at the base&lt;\/p&gt;&lt;p&gt;! Fix the steel cap at the origin along X and Y axes&lt;br&gt;! nsel,s,loc,x,0 ! Select nodes at X = 0 (origin in X)&lt;br&gt;! nsel,s,loc,y,0 ! Select nodes at Y = 0 (origin in Y)&lt;br&gt;! nsel,a,loc,z,l ! Further select nodes at Z = l (end of the cylinder)&lt;\/p&gt;&lt;p&gt;! Apply constraints to the steel cap end nodes&lt;br&gt;! d,all,ux &nbsp; ! Fix displacement in X direction&lt;br&gt;! d,all,uy &nbsp; ! Fix displacement in Y direction&lt;\/p&gt;&lt;p&gt;! Apply pressure on the inner surface of the tube&lt;br&gt;! nsel,s,loc,x,r1 ! Select nodes at the inner radius (r1)&lt;br&gt;! nsel,s,loc,z,0 ! Further select nodes at Z = 0 (base)&lt;br&gt;! nsel,a,loc,z,l ! Include nodes at Z = l (end of the cylinder)&lt;br&gt;! nsel,a,loc,y,0 ! Include nodes at Y = 0 (if required)&lt;br&gt;! sf,all,pres,1000 ! Apply pressure of 1000 Pa (adjust as needed)&lt;\/p&gt;&lt;p&gt;! Apply pressure on the inner surface of the steel cap&lt;br&gt;! nsel,s,loc,x,r2 ! Select nodes at the outer radius (r2) or adjust as needed&lt;br&gt;! nsel,s,loc,z,l ! Select nodes at Z = l (end of the cylinder)&lt;br&gt;! nsel,a,loc,y,0 ! Include nodes at Y = 0 (if required)&lt;br&gt;! sf,all,pres,2000 ! Apply pressure of 2000 Pa (adjust as needed)&lt;\/p&gt;&lt;p&gt;! Solve the model&lt;br&gt;!nsub,5&lt;br&gt;!solv&lt;\/p&gt;&lt;p&gt;! Continue with compression if required&lt;br&gt;! d,nd_top,uz,-u_top ! COMPRESSION ON TOP SURFACE&lt;br&gt;! f,nd_top,fz,-f_top ! COMPRESSION ON TOP SURFACE&lt;br&gt;! nsub,10&lt;br&gt;! solv&lt;br&gt;! Optionally, print material assignments to validate&lt;br&gt;etable,mat,mat &nbsp;! Create a table of material numbers&lt;br&gt;prnsol,etable &nbsp;! Print the table to check material assignment&lt;\/p&gt;&lt;p&gt;&lt;br&gt;fini&nbsp;&lt;\/p&gt;<\/p>\n","protected":false},"template":"","class_list":["post-381315","topic","type-topic","status-publish","hentry"],"aioseo_notices":[],"aioseo_head":"\n\t\t<!-- All in One SEO 4.9.10 - aioseo.com -->\n\t<meta name=\"description\" content=\"Hi everyone I am using Reinf265 with solid 185 as steel wire reinfocements for spiral arrangements of wire along tube.Its a hydraulic tube consists of rubber as base material and 4 layers of steel wire as reinforcements.My model consists of three types of rubber material and steel wire reinforcements.Please comment is smeared reinforcing approach is\" \/>\n\t<meta name=\"robots\" content=\"max-image-preview:large\" \/>\n\t<link rel=\"canonical\" href=\"https:\/\/innovationspace.ansys.com\/forum\/forums\/topic\/reinf265-as-steel-wire-reinfocements-for-spiral-arrangements-apdl\/\" \/>\n\t<meta name=\"generator\" content=\"All in One SEO (AIOSEO) 4.9.10\" 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