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Desired number of eigen-values=%d Dimension of the problem= %d subspace: M[%d][%d] = %e subspace: Zero frequency found! subspace: w[%d] = %e subspace(): Iteration limit exceeded rel. error = %e > %e %4d sub-space iterations, error: %.4e mode: %2d DoF: %5d %9.4lf Hz Make sure that all six rigid body translation are restrained. stodola(): Iteration limit exceeded mode: %2d DoF: %5d %9.4f Hz iter: %4d error: %.4e There are %d modes below %f Hz. ... %d modes were not found. Try increasing the number of modes in order to get the missing modes below %f Hz. ... all %d modes were found. value %e is less than or equal to zero i = %d FRAME version: 6 Dec 2006, GPL Copyright (C) 1992-2006, Henri P. Gavin http://www.duke.edu/~hpgavin/frame/ This is free software with absolutely no warranty. For details, see http://www.fsf.org/copyleft/gpl.html Please enter the input/output file name: %s You entered file name: %s r error: cannot open file '%s' usage: frame infile frame.cln error: cannot open cleaned input file ** %s ** %d %d number of joints nJ = %d number of members nM = %d warning: %d joints and %d members... not enough members to connect all joints. read input doneread loads doneread reactions donea Linear Elastic Analysis ... Temperature Loads Linear Elastic Analysis ... Mechanical Loads Non-Linear Elastic Analysis ... The stiffness matrix is not pos-def. Reduce loads and re-run the analysis. ... NR iter %2d: error = %8.2e %s data check only KdMdKccKcMc%d error in joint coordinate data: joint number out of range Joint: %d %lf %lf %lf %lf error in member property data: Member number out of range Member: %d error in member property data: joint number out of range Member: %d %lf %lf %lf error in member property data: member section property < 0 error in member property data: cross section area is zero error in member property data: a shear area and shear modulus are zero error in member property data: torsional moment of inertia is zero error: cross section bending moment of inertia is zero error : material elastic modulus E or G f is not positive Members must start and stop at different joints member %d J1= %d J2= %d L= %e Perhaps member %d has not been specified. Joint radii are too large. member %d J1= %d J2= %d L= %e r1= %e r2= %e Le= %e %d %d %s %s %lf %d Rember to specify shear deformations with a 0 or a 1 after the member info. Rember to specify geometric stiffness Remember to specify an exageration factor greater than zero w error: cannot open file 'frame.cln' %s number of loaded joints nF = %d error in joint load data: joint number out of range Perhaps you did not specify %d joint loads %lf warning: All joint loads applied at joint %d are zero number of uniform distributed loads nW = %d error: valid ranges for nW is 0 ... %d error in uniform distributed loads: member number %d is out of range warning: All distributed loads applied to member %d are zero number of concentrated member point loads nP = %d error: valid ranges for nP is 0 ... %d error in internal point loads: member number %d is out of range error in point load data: Point load coord. out of range Member: %d L: %lf load coord.: %lf number of members with temperature changes nT = %d error: valid ranges for nT is 0 ... %d error in temperature loads: member number %d is out of range error in thermal load data: section dimension < 0 Member: %d hy: %lf hz: %lf number of joints with reactions nR = %d error: valid ranges for nR is 0 ... %d error in reaction data: joint number %d is greater than the number of joints, %d error in reaction data: Reaction data must be 0 or 1 Data for joint %d, DoF %d is %d error: joint %3d has no reactions Remove joint %3d from the list of reactions and set nR to %3d warning: Un-restrained structure %d imposed reactions. At least 4 reactions are required. error in reaction data: Fully restrained structure %d imposed reactions >= %d degrees of freedom number of joints with prescribed displacements nD = %d Initial displacements can be prescribed only at restrained coordinates joint: %d dof: %d R: %d elastic_K: element stiffness matrix not symetric ... ... k[%d][%d] = %15.6e ... k[%d][%d] = %15.6e ... relative error = %e ... element matrix saved in file 'kt' kt rigid body translations are restrained! RMS matrix error:%9.2e RMS relative equilibrium error: %9.3e number of dynamic modes modes = %d %lf %lf error: Non-positive mass or density d[%d]= %lf BMs[%d]= %lf number of modes to be animated nA = %d nA = %d, only 20 or fewer modes may be animated error: Non pos-def mass matrix M[%d][%d] = %lf number of joints with condensed DoF's nC = %d %d %d %d %d %d %d %d error in matrix condensation data: condensed joint number out of range cj[%d] = %d ... nJ = %d -- FRAME version: 6 Dec 2006, GPL Copyright (C) 1992-2006, Henri P. Gavin -- http://www.duke.edu/~hpgavin/frame/ FRAME is distributed in the hope that it will be useful but with no warranty; for details see the GNU Public Licence: http://www.fsf.org/copyleft/gpl.html %s JOINTS: %d MEMBERS: %d FIXED JOINTS: %d PRESCRIBED DISPLACEMENTS: %d JOINT LOADS: %d UNIFORM MEMBER LOADS: %d CONCENTRATED MEMBER LOADS: %d For 2D problems, the Y-axis is vertical. For 3D problems, the Z-axis is vertical. J O I N T D A T A R E S T R A I N T S Joint X Y Z radius Fx Fy Fz Mx My Mz %5d %14.6f %14.6f %14.6f %8.3f %2d %2d %2d %2d %2d %2d M E M B E R D A T A (local) Member J1 J2 Ax Asy Asz Jxx Iyy Izz E G roll %5d %5d %5d %6.1f %5.1f %5.1f %6.1f %7.1f %7.1f %8.1f %7.1f %3.0f Include shear deformations. Neglect shear deformations. Include geometric stiffness. Neglect geometric stiffness. J O I N T L O A D S + E Q U I V A L E N T J O I N T L O A D S (global) Joint Fx Fy Fz Mxx Myy Mzz %5d %11.3fU N I F O R M M E M B E R L O A D S (local) Member Wx Wy Wz %16.8fC O N C E T R A T E D P O I N T L O A D S (local) Member Px Py Pz x M E M B E R T E M P E R A T U R E C H A N G E S (local) Member coef hy hz Ty+ Ty- Tz+ Tz- %9.2e %9.3fP R E S C R I B E D D I S P L A C E M E N T S (global) Joint Dx Dy Dz Dxx Dyy Dzz E L A S T I C S T I F F N E S S A N A L Y S I S via L D L' decomposition D A T A C H E C K O N L Y * The Stiffness Matrix is not positive-definite * Check that all six rigid-body translations are restrained If geometric stiffness is included, reduce the loads. J O I N T D I S P L A C E M E N T S (global) Joint X-dsp Y-dsp Z-dsp X-rot Y-rot Z-rot 0.0 %11.6fM E M B E R E N D F O R C E S Member Joint Nx Vy Vz Txx Myy Mzz %5d %5d 0.0 %10.3f 0.0 R E A C T I O N S (global) Mxx Myy Mzz 0.0 R M S E Q U I L I B R I U M E R R O R: %9.3e M O D A L A N A L Y S I S R E S U L T S Total Mass: %e Structural Mass: %e J O I N T M A S S E S (diagonal of the mass matrix) (global) Joint X-mass Y-mass Z-mass X-inrta Y-inrta Z-inrta %11.5e Lump masses at joints. Use consistent mass matrix. N A T U R A L F R E Q U E N C I E S & M A S S N O R M A L I Z E D M O D E S H A P E S convergence tolerance: %.3e MODE %5d: f= %lf Hz, T= %lf sec X- modal participation factor = %12.4e Y- modal participation factor = %12.4e Z- modal participation factor = %12.4e Joint X-dsp Y-dsp Z-dsp %11.3eM A T R I X I T E R A T I O N S: %d There are %d modes below %f Hz. error: cannot open meshfile: %s # FRAME ANALYSIS RESULTS http://www.duke.edu/~hpgavin/frame/ # %s # %s# M E S H D A T A (global coordinates) deflection exaggeration: %.1f # Joint X Y Z X-dsp Y-dsp Z-dsp # F L E X E D M E S H D A T A deflection exaggeration: %.1f # X-dsp Y-dsp Z-dsp %5d %11.3e %11.3e %11.3e %11.3e %11.3e %11.3e error: cannot open annotation file: %s # M E S H A N N O T A T I O N F I L E set title "%s\nanalysis file: %s deflection exaggeration: %.1f" set autoscale set noborder set pointsize 1.0 set xtics; set ytics; set ztics; set nozeroaxis set nokey set nolabel # NODE NUMBER LABELS set label ' %d' at %12.4e, %12.4e, %12.4e # MEMBER NUMBER LABELS plot '%s' u 2:3 t 'undeformed mesh' w lp lw 2 lt 1 pt 6 lw 1 lt 5 pt 6, '%s' u 1:2 t 'deformed mesh' w l lw 2 lt 3 %c set parametric %c set view 60, 70, 1 %c set nokey %c set xlabel 'x' %c set ylabel 'y' %c set zlabel 'z' %c splot '%s' u 2:3:4 t 'undeformed mesh' w lp lw 2 lt 1 pt 6 lw 1 lt 5 pt 6, '%s' u 1:2:3 t 'deformed mesh' w l lw 2 lt 3 error: cannot open modal mesh file: %s # M O D E S H A P E D A T A F O R M O D E %d (global coordinates) # deflection exaggeration: %.1f # MODE %5d: f= %lf Hz, T= %lf sec # X- modal participation factor = %12.4e # Y- modal participation factor = %12.4e # Z- modal participation factor = %12.4e # X-dsp Y-dsp Z-dsp error: cannot append annotation file: %s pause -1 set title '%s mode %d %lf Hz' lw 2 lt 1 pt 6 lw 1 lt 5 pt 6, '%s' u 1:2 t 'mode-shape %d' w l lw 2 lt 3 %c pause -1 lw 1 lt 5 pt 6, '%s' u 1:2:3 t 'mode-shape %d' w l lw 2 lt 3 # --- M O D E S H A P E A N I M A T I O N --- set noxtics; set noytics; set noztics; set xrange [ %lf : %lf ] set yrange [ %lf : %lf ] set zrange [ %lf : %lf ] %c set xlabel %c set ylabel %c set zlabel %c set nolabel pause -1 set title '%s mode %d %lf Hz' .plot '%s' u 2:3 w lp lw 1 lt 5 pt 6, '%s' u 1:2 w l lw 2 lt 3 ;%c set view %5.1f, %5.1f, %4.2f %c splot '%s' u 2:3:4 w lp lw 1 lt 5 pt 6, '%s' u 1:2:3 w l lw 2 lt 3; pause 1.5 pause 0.05 %c load 'saveplot'; %c !mv my-plot.ps %s '%s' u 1:2 w l lw 2 lt 3;plot '%s' u 2:3 w lp lw 2 lt 5 pt 6, '%s' u 1:2 w l lw 3 lt 3 %c splot '%s' u 2:3:4 w lp lw 2 lt 5 pt 6, '%s' u 1:2:3 w l lw 3 lt 3 # A N I M A T E D M O D E S H A P E D A T A # deflection exaggeration: %.1f # MODE %5d: f= %lf Hz T= %lf sec j1 = %d j2 = %d L = %e u7 = %e %12.4e %12.4e %12.4e ldl_dcmp(): zero found on diagonal ... d[%d] = %11.4e pseudo_inv: warning beta = %lf lu_dcmp: zero found on the diagonal A[%d][%d] = %11.4e Numerical Recipes run-time error... ...now exiting to system... nl = %d nh = %d allocation failure in vector()allocation failure in ivector()allocation failure in Cvector()allocation failure in dvector()allocation failure 1 in matrix()allocation failure 2 in matrix()alloc failure 1 in 3Dmatrix()alloc failure 2 in 3Dmatrix()alloc failure 3 in 3Dmatrix()allocation failure 1 in Cmatrix()allocation failure 2 in Cmatrix()allocation failure 1 in dmatrix()allocation failure 2 in dmatrix()allocation failure 1 in imatrix()allocation failure 2 in imatrix()allocation failure in submatrix()allocation failure in convert_matrix()%14.6e 0 ]; %11.3e error: cannot open file: %s %15.6e 0 %14d 0 0 %21.12e 0 $?? @?-DT!@?0.++Y@-DT! @f@(@@@@@ư>333333??$$@?*@A@@@Z@.@&@j@&@@z@*"@Q@a@>EN}a+k4$d" -?d #@d #Yd #w<. #D #D#D!#D*#D3#D?#DA#DM#DO#DT#DY#Dn#Du#D}#D#D#D#D#D#D#D #D#D#$ # @"1@:E #F $GVe$N $f $. $D+ $D.$D0*$D1-$|$+ $, $3$$*N3$ - . / 0d3$    8@$K #\4$[YaZ   =HEH,  MT{']nz,: 0 4 8iI+ <@^`CL\> @X Ds H L P T X \ IgY}FsG`S   _`^_$`^y^.4_<G^9^FE`V.^&py/zCjX\JGXz08I)3MaTP+R JDEcYZh/nzf kWyjNuo@{[X `=T4gtefj0jhdcabaV6UG]F$[X