M M W W MMMMM MMMMM WWWWW WWWWW MMMMMMMMM MMMMMMMMM WWWWWWWWW WWWWWWWWW MMMMMMMMMMMMM MMMMMMMMMMMMM WWWWWWWWWWWWW WWWWWWWWWWWWW MMMMMMMMMMMMMMMMMMMMMMMMMMMMMMMMM WWWWWWWWWWWWWWWWWWWWWWWWWWWWWWWWW MMMMMMMM MMMMMMMMMMMMMMM MMMMMMMM WWWWWWWW WWWWWWWWWWWWWWW WWWWWWWW MMMMMM MMMMMMMMMMM MMMMMM WWWWWW WWWWWWWWWWW WWWWWW MMMM MMMMMMM MMMM WWWW WWWWWWW WWWW MM MMM MM WW WWW WW M M M W W W MM MMM MM WW WWW WW MMMM MMMMMMM MMMM WWWW WWWWWWW WWWW MMMMMM MMMMMMMMMMM MMMMMM WWWWWW WWWWWWWWWWW WWWWWW MMMMMMMM MMMMMMMMMMMMMMM MMMMMMMM WWWWWWWW WWWWWWWWWWWWWWW WWWWWWWW MMMMMMMMMMMMMMMMMMMMMMMMMMMMMMMMM WWWWWWWWWWWWWWWWWWWWWWWWWWWWWWWWW MMMMMMMMMMMMM MMMMMMMMMMMMM WWWWWWWWWWWWW WWWWWWWWWWWWW MMMMMMMMM MMMMMMMMM WWWWWWWWW WWWWWWWWW MMMMM MMMMM WWWWW WWWWW M M W W version: MSC.Marc (forming) based on Build 34405, December 08 2005, Build: 2007-08-21 machine type: NT integer*4 version: integers are 32-bits date: Mon Nov 5 11:14:41 2007 (c) COPYRIGHT 2005 MSC.Software Corporation, all rights reserved MSC.Marc (forming) - N T i n p u t d a t a p a g e 1 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 ---------------------------------------------------------------------------------------------------------------------------------------------------------------- title job3 $....sfFormingSFM input file produced by sfFormingSFM 8.0 (32bit) $................................... $....input file using extended precision card 5 extended $................................... sizing 0 7889 8472 3 alloc 25 elements 10 card 10 version 11 processor 1 1 1 0 ---------------------------------------------------------------------------------------------------------------------------------------------------------------- 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 ---------------------------------------------------------------------------------------------------------------------------------------------------------------- ---------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 general memory increasing from 25 MByte to 53 MByte memory increased to 14001931 words during pre-reading of sets allocated workspace of 13 words of memory for body 1 allocated workspace of 13 words of memory for body 2 allocated workspace of 13 words of memory for body 3 allocated workspace of 13 words of memory for body 4 allocated workspace of 13 words of memory for body 5 allocated workspace of 13 words of memory for body 6 allocated workspace of 13 words of memory for body 7 allocated workspace of 13 words of memory for body 8 allocated workspace of 13 words of memory for body 9 allocated workspace of 13 words of memory for body 10 allocated workspace of 13 words of memory for body 11 1 ************************************************* ************************************************* program sizing and options requested as follows element type requested************************* 10 number of elements in mesh********************* 7889 number of nodes in mesh************************ 8472 max number of elements in any dist load list*** 0 maximum number of point loads****************** 0 large displacement analysis flagged************ load correction flagged or set***************** number of lists of distributed loads*********** 3 values stored at all integration points******** tape no.for input of coordinates + connectivity 5 boundary conditions applied on current geometry no.of different materials 3 max.no of slopes 17 number of points on shell section ************* 11 geometry updated after each load step********** formulation for large strain plasticity ******* new style input format will be used************ mesh rezoning option is switched on************ triangular interpolation is used*************** number of processors used ********************* 1 MSC.SuperForm analysis performed ************** initial stress stiffness neglected ************ constant dilatation formulation is used ******* incremental plasticity - mean normal method used extended precision input is used ************** MSC.Marc input version ************************ 11 system uses SI-millimeter unit: mm,N,s,C suppress echo of list items ******************* suppress echo of bc summary ******************* suppress echo of nurbs data ******************* end of parameters and sizing ************************************************* ************************************************* 1 key to stress, strain and displacement output element type 10 4-node isoparametric quadrilateral ring stresses and strains in global directions 1=zz 2=rr 3=hoop 4=zr displacements in global directions 1=u axial direction 2=v radial direction allocated 16944 words of memory due to shell, user or contact transformations workspace needed for input and stiffness assembly: 334121 internal core allocation parameters degrees of freedom per node (ndeg) 2 max. number of coordinates per node 2 max. nodes per element (nnodmx) 4 max. invariants per int. points (neqst) 1 max.stress components per int. point (nstrmx) 4 strains per integration point (ngens) 4 flag for element storage (ielsto) 0 element data in core memory usage per element group group # elements nelsto MByte words 1 3276 570 7 1867320 2 3945 570 9 2248650 3 668 570 1 380760 ---------------------------------------------------------- total 7889 17 4496730 internal element variables internal element number 1 library code type 10 number of nodes= 4 stresses stored per integration point = 4 direct continuum components stored = 3 shear continuum components stored = 1 shell/beam flag = 0 curvilinear coord. flag = 0 int.points for elem. stiffness 4 number of local inertia directions 2 int.point for print if all points not flagged 5 int. points for dist. surface loads (pressure) 2 library code type = 10 large disp. row counts 4 4 2 7 residual load correction is invoked $................... solver ---------- multifrontal direct sparse solver invoked solution of non-positive definite equation systems will be forced optimize 11 ---------- metis nested dissection algorithm connectivity ---------- meshr1, iprnt 5 1 elem no., type, nodes coordinates ---------- ncrd1 ,meshr1,iprnt 2 5 1 node coordinates define element set Dorn ---------- from element 3277 to element 5764 by 1 define element set Huelse ---------- from element 1 to element 3276 by 1 define node set NH_y_fest_nodes ---------- a list of nodes given below 1 define node set NH_x_fest_nodes ---------- a list of nodes given below 1 define node set temp_Dorn_oben_nodes ---------- from node 1 to node 8472 by 1 define body set NH_heran_fcbodys ---------- a list of bodies given below 3 4 7 define body set NH_heran_mcbodys ---------- a list of bodies given below 6 define body set Zug_heran_fcbodys ---------- a list of bodies given below 3 4 6 define body set Zug_heran_mcbodys ---------- a list of bodies given below 7 define body set Zug_weg_cbodys ---------- a list of bodies given below 7 define body set NH_weg_mcbodys ---------- a list of bodies given below 6 define body set NH_weg_fcbodys ---------- a list of bodies given below 3 4 7 define body set Zug_weg_fcbodys ---------- a list of bodies given below 3 4 6 define body set Zug_weg_mcbodys ---------- a list of bodies given below 7 define element set Dorn_oben ---------- from element 5765 to element 7221 by 1 define body set Dorntrennung_cbodys ---------- a list of bodies given below 5 define node set NH_weg_nodes ---------- a list of nodes given below 1 define element set oberes_Blech ---------- from element 7222 to element 7470 by 1 define element set unteres_Blech ---------- from element 7471 to element 7889 by 1 define body set NH_weg_cbodys ---------- a list of bodies given below 6 define body set Klemmkraft_oben_heran_fcbodys ---------- a list of bodies given below 6 7 9 define body set Klemmkraft_oben_heran_mcbodys ---------- a list of bodies given below 8 define body set Klemmkraft_unten_heran_fcbodys ---------- from body 6 to body 8 by 1 define body set Klemmkraft_unten_heran_mcbodys ---------- a list of bodies given below 9 define body set NH_weg_haften_cbodys ---------- a list of bodies given below 6 define body set NH_weg_haften_fcbodys ---------- a list of bodies given below 3 4 7 define body set NH_weg_haften_mcbodys ---------- a list of bodies given below 6 define body set Dorntrenn_haften_cbodys ---------- a list of bodies given below 5 isotropic ---------- isotropic material material id = 1 von mises yield criteria isotropic hardening rule material name is: Huelsenmat property value Youngs modulus 2.10000E+05 Poissons ratio 3.00000E-01 mass density 1.00000E+00 shear modulus 8.07692E+04 coefficient of thermal expansion 0.00000E+00 Yield stress 3.50000E+02 fraction contribution to kinematic hard. 0.00000E+00 cost per unit volume 0.00000E+00 cost per unit mass 0.00000E+00 from element 1 to element 3276 by 1 work hard data ---------- no. of points for primary curve is 17 for secondary curve is 0 material id 1 read from unit 5 yield stress equivalent plastic strain 3.50000E+02 0.00000E+00 3.59497E+02 1.00000E-02 3.87425E+02 2.00000E-02 4.27768E+02 5.00000E-02 4.61105E+02 1.00000E-01 4.97082E+02 2.00000E-01 5.35911E+02 4.00000E-01 5.77816E+02 8.00000E-01 5.92000E+02 1.00000E+00 6.03851E+02 1.20000E+00 6.14058E+02 1.40000E+00 6.27162E+02 1.70000E+00 6.38349E+02 2.00000E+00 6.48130E+02 2.30000E+00 6.56835E+02 2.60000E+00 6.62154E+02 2.80000E+00 6.67145E+02 3.00000E+00 isotropic ---------- isotropic material material id = 2 von mises yield criteria isotropic hardening rule material name is: Dornmat property value Youngs modulus 2.10000E+05 Poissons ratio 3.00000E-01 mass density 1.00000E+00 shear modulus 8.07692E+04 coefficient of thermal expansion 0.00000E+00 Yield stress 1.10000E+03 fraction contribution to kinematic hard. 0.00000E+00 cost per unit volume 0.00000E+00 cost per unit mass 0.00000E+00 from element 3277 to element 7221 by 1 work hard data ---------- no. of points for primary curve is 17 for secondary curve is 0 material id 2 read from unit 5 yield stress equivalent plastic strain 1.10000E+03 0.00000E+00 1.13915E+03 1.00000E-02 1.19349E+03 2.00000E-02 1.27136E+03 5.00000E-02 1.33519E+03 1.00000E-01 1.40361E+03 2.00000E-01 1.47693E+03 4.00000E-01 1.55552E+03 8.00000E-01 1.58200E+03 1.00000E+00 1.60408E+03 1.20000E+00 1.62306E+03 1.40000E+00 1.64740E+03 1.70000E+00 1.66813E+03 2.00000E+00 1.68623E+03 2.30000E+00 1.70232E+03 2.60000E+00 1.71214E+03 2.80000E+00 1.72135E+03 3.00000E+00 isotropic ---------- isotropic material material id = 5 von mises yield criteria isotropic hardening rule material name is: H260 property value Youngs modulus 2.10000E+05 Poissons ratio 3.00000E-01 mass density 1.00000E+00 shear modulus 8.07692E+04 coefficient of thermal expansion 0.00000E+00 Yield stress 2.90140E+02 fraction contribution to kinematic hard. 0.00000E+00 cost per unit volume 0.00000E+00 cost per unit mass 0.00000E+00 from element 7222 to element 7889 by 1 work hard data ---------- no. of points for primary curve is 12 for secondary curve is 0 material id 5 read from unit 5 yield stress equivalent plastic strain 2.90140E+02 0.00000E+00 3.06013E+02 1.00000E-02 3.30331E+02 2.00000E-02 3.53364E+02 3.00000E-02 3.71735E+02 4.00000E-02 3.86850E+02 5.00000E-02 4.10327E+02 7.00000E-02 4.35719E+02 1.00000E-01 4.54751E+02 1.30000E-01 4.70135E+02 1.60000E-01 5.00000E+02 2.50000E-01 5.00000E+02 8.00000E-01 fixed disp ---------- fixed displacement = 0.000E+00 0.000E+00 a list of degrees of freedom given below 2 a list of nodes given below 1 allocated 950 words of memory due to kinematic boundary conditions fixed displacement = 0.000E+00 0.000E+00 a list of degrees of freedom given below 1 a list of nodes given below 1 fixed displacement = -1.000E-01 0.000E+00 a list of degrees of freedom given below 1 a list of nodes given below 1 fixed boundary condition summary. total fixed degrees of freedom read so far = 3 initial temp ---------- number of series used for initial temperatures is 0 read from unit 5 initial value 2.0000000E+01 from node 1 to node 8472 by 1 adapt global ---------- number of remeshing regions/bodies 3 adaptive remeshing method: Quadtree mesher body 1 number of remeshing criteria : 3 remesh at increment frequency: 4 element distortion criterion used maximum strain change criterion used maximum strain since last remesh allowed is 0.400000 atom size in x-direction 6.00000E-02 atom size in y-direction 6.00000E-02 coarsening flag 2 refine flag 2 number of elements control : 0 =0.0 - default - controlled by target size curvature measure 0.001000 user defined parameters are 1 0 0 user defined parameters are 6.000000E-02 2.000000E+00 0.000000E+00 remeshing control variables mesh quality 0.30000E+00 corner edge angle 0.60000E+02 number of shakes 4 number of runs 0 trimming control variables trimming parameter 4 inner radius 0.80000E-01 outer radius 0.00000E+00 adaptive remeshing method: Quadtree mesher body 2 number of remeshing criteria : 2 element distortion criterion used maximum strain change criterion used maximum strain since last remesh allowed is 0.400000 atom size in x-direction 8.00000E-02 atom size in y-direction 8.00000E-02 coarsening flag 2 refine flag 2 number of elements control : 0 =0.0 - default - controlled by target size curvature measure 0.001000 user defined parameters are 1 0 0 user defined parameters are 6.000000E-02 2.000000E+00 0.000000E+00 remeshing control variables mesh quality 0.30000E+00 corner edge angle 0.60000E+02 number of shakes 3 number of runs 0 trimming control variables trimming parameter 3 inner radius 0.80000E-01 outer radius 0.00000E+00 adaptive remeshing method: Quadtree mesher body 5 number of remeshing criteria : 0 atom size in x-direction 1.00000E-01 atom size in y-direction 1.00000E-01 coarsening flag 0 refine flag 0 number of elements control : 0 =0.0 - default - controlled by target size curvature measure 0.001000 user defined parameters are 0 0 0 user defined parameters are 0.000000E+00 0.000000E+00 0.000000E+00 remeshing control variables mesh quality 0.30000E+00 corner edge angle 0.60000E+02 number of shakes 3 number of runs 0 trimming control variables trimming parameter 3 inner radius 0.00000E+00 outer radius 0.00000E+00 contact ---------- number of bodies = 11 shear friction with atan function regularization selected (type 3) friction calculations based on nodal stresses no increment splitting during analysis separation based upon average nodal stresses: nodal stress is calculated as force divided by effective area separation threshold is treated as a stress suppress contact surface print out *** warning - the relative sliding velocity below which sticking is simulated will be estimated based on the local relative sliding velocity relative velocity below which a node is considered sticking = 0.00000E+00 distance below which a node is considered touching a surface = 0.00000E+00 separation threshold = 2.00000E+01 contact bias factor = 9.50000E-01 $....contact body 1: Huelse body number = 1 body name = Huelse number of sets of data = 0 single sided contact used body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 from element 1 to element 3276 by 1 $....contact body 2: Dorn body number = 2 body name = Dorn number of sets of data = 0 single sided contact used body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 from element 3277 to element 5764 by 1 $....contact body 3: oberes_Blech body number = 3 body name = oberes_Blech number of sets of data = 0 single sided contact used body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 from element 7222 to element 7470 by 1 $....contact body 4: unteres_Blech body number = 4 body name = unteres_Blech number of sets of data = 0 single sided contact used body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 from element 7471 to element 7889 by 1 $....contact body 5: Dorn_oben body number = 5 body name = Dorn_oben number of sets of data = 0 single sided contact used body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 from element 5765 to element 7221 by 1 $....contact body 6: Niederhalter body number = 6 body name = Niederhalter number of sets of data = 1 single sided contact used body number 6 is a load-controlled surface and attaches to node numbers 1 0 body positioning data 1st coordinate of center of rotation 5.11815E+00 2nd coordinate of center of rotation 5.40000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 friction coefficient 0.00000E+00 data internally reduced to 4 segments allocated workspace of 89 words of memory for body 6 $....contact body 7: Zugwerkzeug body number = 7 body name = Zugwerkzeug number of sets of data = 1 single sided contact used body number 7 is a velocity controlled rigid surface body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 data internally reduced to 4 segments allocated workspace of 89 words of memory for body 7 $....contact body 8: Klemmkraft_oben body number = 8 body name = Klemmkraft_oben number of sets of data = 1 single sided contact used body number 8 is a velocity controlled rigid surface body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 data internally reduced to 25 segments allocated workspace of 488 words of memory for body 8 $....contact body 9: Klemmkraft_unten body number = 9 body name = Klemmkraft_unten number of sets of data = 1 single sided contact used body number 9 is a velocity controlled rigid surface body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 data internally reduced to 28 segments allocated workspace of 545 words of memory for body 9 $....contact body 10: symmetrie body number = 10 body name = symmetrie number of sets of data = 1 single sided contact used body number 10 is a velocity controlled rigid surface body number 10 is a symmetry plane body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 data internally reduced to 1 segments allocated workspace of 32 words of memory for body 10 $....contact body 11: symmetrie2 body number = 11 body name = symmetrie2 number of sets of data = 1 single sided contact used body number 11 is a velocity controlled rigid surface body number 11 is a symmetry plane body positioning data 1st coordinate of center of rotation 0.00000E+00 2nd coordinate of center of rotation 0.00000E+00 initial angle rotated around axis 0.00000E+00 1st component of approach velocity 0.00000E+00 2nd component of approach velocity 0.00000E+00 angular approach velocity 0.00000E+00 1st component of velocity 0.00000E+00 2nd component of velocity 0.00000E+00 angular velocity 0.00000E+00 friction coefficient 0.00000E+00 data internally reduced to 1 segments allocated workspace of 32 words of memory for body 11 no print ---------- restart last ---------- last increment read from unit 9 reauto ---------- time step size: 0.0000000E+00 end value of time: 0.0000000E+00 maximum number of steps: 1 reassembly interval: 0 desired recycles: 0 maximum stepsize: 0.0000000E+00 current loading factor: 0.0000000E+00 post ---------- number of element variables on post file: 7 binary post file will be used initial output frequency of post file: 1 MSC.Marc 2005 style post file post variable 1 is post code 7 = post variable 2 is post code 18 = post variable 3 is post code 28 = post variable 4 is post code 90 = post variable 5 is post code 301 = post variable 11 is post code 311 = post variable 17 is post code 321 = maximum record length on binary post file= 8472 approximate no. of words per increment on file= 694248 post option is behind restart option - old post tape will be copied onto beginning of new post tape Nodal post code 1 = Nodal post code 28 = Nodal post code 34 = Nodal post code 36 = Nodal post code 38 = parameters ---------- parameters set as follows predictor used for stress-strain calculation 1.00000E+00 penalty factor for boundary conditions 1.00000E+09 penalty for incompressibility - r-p flow 1.00000E+02 penalty for incompressibility - fluid flow 1.00000E+06 beta parameter for Newmark operator 2.50000E-01 gamma parameter for Newmark operator 5.00000E-01 gamma1 parameter for Single-Step-Houbolt 1.50000E+00 gamma parameter for Single-Step-Houbolt -5.00000E-01 sharp angle for sticking/separating - 2D 8.62500E+00 sharp angle for sticking/separating - 3D 2.00000E+01 initial strain rate for r-p flow 1.00000E-04 lowest strain rate cutoff for r-p flow 1.00000E-06 fraction of dilatational stress neglected 1.00000E+00 factor for drilling d.o.f for shells 1.00000E-04 factor for displacement after rezoning 1.00000E+00 universal gas constant 8.31400E+03 absolute temperature offset 2.73150E+02 thermal properties evaluation weight 5.00000E-01 surface projection factor in ssh dynamics 0.00000E+00 Stefan Boltzmann constant 5.67051E-11 Planck's second radiation constant 1.43877E-02 Speed of light in vacuum 2.99790E+08 maximum iterative displacement component 1.00000E+30 initial stiffness to simulate sticking 0.00000E+00 end option ---------- solution of non-positive definite equation systems will be forced direct symmetric multi-frontal sparse solver is invoked for region 1 number of element groups used: 3 group # elements element type material 1 3276 10 1 2 3945 10 2 3 668 10 5 **** note **** can not find the following flow-data file in job directory or in the material library: C:\PROGRA~1\Femutec\simufact\forming\8.0\sfMarc\tools\..\AF_flowmat\Huelsenmat.mat This is ok if no separate flow-data file is required. Otherwise please provide the data file or result will be wrong. **** note **** can not find the following flow-data file in job directory or in the material library: C:\PROGRA~1\Femutec\simufact\forming\8.0\sfMarc\tools\..\AF_flowmat\Dornmat.mat This is ok if no separate flow-data file is required. Otherwise please provide the data file or result will be wrong. **** note **** can not find the following flow-data file in job directory or in the material library: C:\PROGRA~1\Femutec\simufact\forming\8.0\sfMarc\tools\..\AF_flowmat\H260.mat This is ok if no separate flow-data file is required. Otherwise please provide the data file or result will be wrong. **now reading increment 91. 0 from restart file** **now reading increment 91. 0 from restart file** allocated 62860 words of memory due to shell, user or contact transformations allocated 4978 words of memory due to shell, user or contact transformations allocated 5250 words of memory due to tyings allocated 5567 words of memory due to kinematic boundary conditions allocated workspace of 47673 words of memory for body 1 allocated workspace of 30981 words of memory for body 2 allocated workspace of 8097 words of memory for body 3 allocated workspace of 22209 words of memory for body 4 allocated workspace of 29949 words of memory for body 5 restart at increment 91. 0 $................... $....start of loadcase Dorntrennung title Dorntrennung ---------- adapt global ---------- number of remeshing regions/bodies 3 adaptive remeshing method: Quadtree mesher body 1 number of remeshing criteria : 4 remesh at increment frequency: 4 element distortion criterion used maximum strain change criterion used maximum strain since last remesh allowed is 0.400000 force remeshing to occur atom size in x-direction 6.00000E-02 atom size in y-direction 6.00000E-02 coarsening flag 2 refine flag 2 number of elements control : 0 =0.0 - default - controlled by target size curvature measure 0.001000 user defined parameters are 1 0 0 user defined parameters are 6.000000E-02 2.000000E+00 0.000000E+00 remeshing control variables mesh quality 0.30000E+00 corner edge angle 0.60000E+02 number of shakes 4 number of runs 0 trimming control variables trimming parameter 4 inner radius 0.80000E-01 outer radius 0.00000E+00 adaptive remeshing method: Quadtree mesher body 2 number of remeshing criteria : 3 element distortion criterion used maximum strain change criterion used maximum strain since last remesh allowed is 0.400000 force remeshing to occur atom size in x-direction 8.00000E-02 atom size in y-direction 8.00000E-02 coarsening flag 2 refine flag 2 number of elements control : 0 =0.0 - default - controlled by target size curvature measure 0.001000 user defined parameters are 1 0 0 user defined parameters are 6.000000E-02 2.000000E+00 0.000000E+00 remeshing control variables mesh quality 0.30000E+00 corner edge angle 0.60000E+02 number of shakes 3 number of runs 0 trimming control variables trimming parameter 3 inner radius 0.80000E-01 outer radius 0.00000E+00 adaptive remeshing method: Quadtree mesher body 5 number of remeshing criteria : 1 force remeshing to occur atom size in x-direction 1.00000E-01 atom size in y-direction 1.00000E-01 coarsening flag 0 refine flag 0 number of elements control : 0 =0.0 - default - controlled by target size curvature measure 0.001000 user defined parameters are 0 0 0 user defined parameters are 0.000000E+00 0.000000E+00 0.000000E+00 remeshing control variables mesh quality 0.30000E+00 corner edge angle 0.60000E+02 number of shakes 3 number of runs 0 trimming control variables trimming parameter 3 inner radius 0.00000E+00 outer radius 0.00000E+00 continue ----------