1-5233716 2001.0.9 Dynamics - MEFFMASS - UFM 2025 (EFFMAS) In a large model that has many coordinate systems and requesting effective mass output (MEFFMASS), the job may fail with the following error messages *** USER FATAL MESSAGE 2025 (EFFMAS) UNDEFINED COORDINATE SYSTEM ID = xxxx *** SYSTEM INFORMATION MESSAGE 1156 (XCLNUP) GINO FILE 301 WAS LEFT OPEN AT PROGRAM TERMINATION. This error occurs even though the coordinate system referenced in the message exists. Avoidance: The effmass.v707 alter from the v70.7 sssalter library provides similar output and this alter will run in v2001 also. Removing unused CORD2R entries may also allow the job to run successfully. 1-5469524 2001.0.9 Nonlinear Analysis - TET10 - Possible Wrong Answers When using the nonlinear tet10 elements, if the material is elastic perfectly plastic and the default grid option is used, then the stresses may be incorrect. Avoidance: Use the GAUSS option by specifying GAUSS in field 6 of the PSOLID entry. 1-5931701 2001.0.9 Nonlinear Analysis - TET10, PLASTIC - UFM 4551 (NCONVG) The TET10 element has problems converging in nonlinear analysis in the plastic range. This problem may lead to the following fatal message: *** USER FATAL MESSAGE 4551 (NCONVG) *** STOPPED PROBLEM DUE TO FAILED CONVERGENCE Avoidance: The problems has been corrected in Version 2001.0.9 available on the Nastran 2001 R4 CD. 1-6521817 2001.0.9 Heat Transfer - RMG2 - SFM 4276, Traceback Very large heat transfer jobs that calculate large view factors may fail with a traceback in rmg2. Avoidance: The failure occurs when the memory requirement is calculated and overflows. There is no avoidance. 1-6953959 2001.0.9 Loads - OLOAD and SPCFORCE Resultant Output Incorrect use param,resltopt,1 to get correct The oload and spcforce resultants are incorrect in v2001.0.4 and later systems if global coordinate systems are present and loads and/or spcs are applied to grid points that reference an output coordinate system. Avoidance: Use param,resltopt,1 to get correct results but in the old format 1-7055609 2001.0.9 Aeroelastic Analysis - Flutter roots not sorted for the PKNL method The sorting of flutter roots that is used for the PK and PKNL is disabled when the density used in the analysis changes. Since the PKNL method is likely to change the density value for each analysis triplet, this effectively means that the roots are not sorted. Avoidance: Use the PK method or perform the sorting as a post-processing operation. 1-7510324 2001.0.9 Aeroelastic Analysis - Different Flutter Solutions for Supersonic Speeds The AMG module generates a different aerodynamic matrix across different machine types for supersonic Mach numbers. The largest difference was found on Windows/NT and the HPUX(64-bit) machines. Avoidance: There is no avoidance. 1-7514301 2001.0.9 Optimization/Design Sensitivities - PCOMP - Wrong Answers A composite optimization job may produce incorrect sensitivities when the following two conditions are met: 1) Any material properties referenced by PCOMP entries are being designed; 2) The designed PCOMPs are referenced by more than one composite elements. In addition, when a dummy PCOMP is present, the sensitivity coefficients may also be incorrect. Avoidance: There is no avoidance for the first case. However, for the case of a dummy PCOMP entry, rename the PID to the smallest number among all PCOMP IDs. 1-7734165 2001.0.9 Aeroelastic Analysis - AESURF - Missing Output The printed output of the INERTIAL nondimensional hinge moment derivative coefficients may not print in the proper table of the output in the f06 file. If some AESURF entries have associated AESURFS entries and there are other AESURF entries without associated AESURFS entries having identification numbers lower than the AESURF with AESURFS, then the printed output of the nondimensional hinge moment derivative coefficients will NOT appear in the appropriate table in the f06 results. Avoidance: The only avoidance is to renumber the AESURF entries.