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Grip Point Force Balance, Freebody Load

- February 16, 2026 at 3:45 pm
  
  e195027
  Subscriber
  
  Hi,
  Based on a static analysis, we can generate a freebody load (GPFORCE) on the desired node in MSC Nastran.
  How can we do this in Ansys? Can you help me?
  I'm attaching a screenshot of a simple GPFORCE generated on a Nastran plate.
  
  Thanks
- February 16, 2026 at 10:23 pm
  
  peteroznewman
  Subscriber
  
  Nastran provides very little output unless you specifically request it. Ansys provides lots of output unless you specifically turn it off, however Nodal Forces is one output that is off by default so if you are solving in the Workbench/Mechanical environment, go to Analysis Settings, Output Controls and Set Nodal Forces to Yes before you solve.
  Here is an Ansys model with the same loads and boundary conditions you show, which are generally applied to geometry in Ansys Workbench/Mechanical.
  There are two places you might want to sum up the Nodal Forces (Grid Point Forces in Nastran): 1. At boundary conditions and 2. at an arbitrary plane.
  To get the sum of Nodal Forces at a boundary condition,under the Solution branch insert Probe > Force Reaction and select the Fixed Support BC.
  To get the Nodal Forces at an arbitrary plane, first insert and position the XY plane of a coordinate system where you want to cut your mesh. Then under Geometry insert a Construction Surface using that coordinate system.
  Then insert another Probe > Force Reaction result, but change the Location Method to Surface, pick the surface then pick the Geometry that was meshed and select the Extraction to be on the Positive side or the Negative side of the surface. Below you can see the color code on the three nodes are 442.85 N at the center and 278.57 N at the edges.
  To get results at a different location, simply edit the global coordinates of the coordinate system you created and the results will update without a new solution.
- February 17, 2026 at 12:17 am
  
  e195027
  Subscriber
  
  Thank you for your reply and interest. First, let me give you some information about the model I prepared:
  Plate size is 50x100x1mm
  Element size is 25mm
  Material allowables for all:
  Young’s Modulus is 70000MPa
  Poisson’s ratio is 0.33
  
  As you said, we can read the reaction force from any node we want. When we get the GPFB output in Nastran, we get 2 force and 1 moment values. When we get these, we select the 2 shell elements and 1 node element in front of the node from which we want to get the GPFB, and calculate the GPFB. As a result, it gives us the normal reaction force, the bending moment, and the force in the x-direction.
  
  In Ansys, we could only read this where we kept it as a fix because in the fix location, there were only 2 shell elements in front of the selected node, and it gave the same result as Nastran. However, when we wanted the same output for the node one node in front of the fix location, we could not get the same result with Nastran. Also, we used APDL to obtain these results. Is it possible to create the model I attached in ANSYS and obtain these values from the nodes in the results I attached?
  Thank you.
- February 17, 2026 at 12:40 am
  
  e195027
  Subscriber
  
  Actually, I want to plot net loads at structure interface.
- February 17, 2026 at 1:02 am
  
  e195027
  Subscriber
- February 17, 2026 at 2:39 am
  
  peteroznewman
  Subscriber
  
  Here is an Ansys model with a beam and shell elements sharing nodes.
  I created a Named Selection for the once vertex and a Nodal Named Selection for Node-Fixed and used that in the Probe > Reaction Force using Location Method Named Selection.
- February 17, 2026 at 7:53 am
  
  e195027
  Subscriber
  
  Hi,
  Thank you for your reply.
  As said before, we can get same results at fixed support but for the node in front of the fixed support we cannot get the same results Nastran. I dont want to get reaction force, I need GPFB at a specific location.
  Here is the ANSYS results in front of the fixed support node;
- February 17, 2026 at 8:54 am
  
  e195027
  Subscriber
  
  While using the force reaction and moment reaction with surfaces, we cannpt select plate body and 1-D beam body at the same time.
- February 17, 2026 at 4:30 pm
  
  peteroznewman
  Subscriber
  
  Plot the Directional Deformation on your model and I think it will become clear that your shell and beam elements are not connected. They are both supported at the fixed end, but seem to not be connected at the free end and the force is only applied to a node on the beam element while there is a coincident node on the shell element that has no load.
  Look at the deformed shape where the beam is passing through the plate. If you change the sign on the Force, you will see those two bodies separating instead of penetrating.
  
  One corrective action in your model is to insert under the Mesh a Node Merge Group type a tolerance value to equivalence the nodes and Generate the result. Now when you solve, you should see the beam and shell elements moving together on shared nodes. I accomplish the same result by using the Share button in SpaceClaim to tell the Ansys mesher to share nodes instead of create coincident nodes. Here is my mesh with the nodes turned on.
  When I insert a Force Reaction at Node 7, Ansys reports a near zero value because it sums up the forces from all elements attached to that node and is should sum to near zero.
  Now I haven't lost sight of your original question, I understand you want a table that breaks down the forces coming from the beam elements in one bucket, and the forces coming from the shell elements in another bucket (or something like that), so I will try to address that in my next reply.
  Please reply with the Nastran .dat or .bdf lines that represents the model you described above. I will take a look at the Nastran output. Format the Nastran lines of text in your reply using the Preformated setting instead of the default Paragraph (accessible in the toolbar at the bottom of the reply) in order to skip turning each line into a Paragraph.
- February 17, 2026 at 9:42 pm
  
  peteroznewman
  Subscriber
  
  Another observation on your Nastran model is that the shell elements have half their thickness above the node and half below, while the I-beam profile is only above the node. In reality, the stiffner sits on the top face of the plate, so it would be more accurate to offset the shell element by 0.5 mm to have it connect to the I-beam at the correct height.
  In the next version of the Ansys model, I moved the plate down by 0.5 mm so that the stiffener is now located above the plate thickness instead of halfway through the thickness.
  When I turn off Thick Plates and Shells, you see that the plates have nodes along the center and the beam has separate nodes above the plate nodes.
  I used what Nastran would call an RBE2 element and Ansys calls a Fixed Joint to connect the five pairs of adjacent nodes.
  After solving, I can extract the forces and moments going through each joint element. Here is the result for the force going through node 17 at flag B above.
  Ansys has a Report Preview on the Home tab where a table of all the Probes with the results is listed.
  You can get all 5 joints if you want.
- February 18, 2026 at 7:54 am
  
  e195027
  Subscriber
  
  Hi,
  Thank you for your reply.
  here is the bdf file :
  
  $
  $ $ Created by MSC Apex Version 2024.2 on Feb 13, 2026 at 19:19:12
  $
  $ Values exported in this file are expressed using the consistent SI_mm_t_deg
  $ unit system
  $ Length mm
  $ Mass t
  $ Time s
  $ Force N
  $ Temperature K
  $ NOTE: Nastran requires the following angle values always be defined in
  $ degrees, while all other rotational quantities will be defined in terms of
  $ radians
  $ PCOMPG (THETAi - ply orientation angle)
  $ TABLED1 (yi - phase angle data when referenced in TP field of RLOAD2)
  $
  $ Linear Static Scenario Static Scenario Model Assembly
  $ Scenario description
  SOL 101
  CEND
  PARAM,AUTOMSET,AUTO
  $ Automatic Stiffness Singularity Constraints
  AUTOSPC(NOPRINT) = YES
  ECHO=NONE
  $
  $ Output Requests
  $
  DISPLACEMENT(PLOT) = ALL
  STRESS(PLOT,VONMISES,CORNER) = ALL
  OLOAD(PLOT) = ALL
  SPCFORCES(PLOT) = ALL
  GPFORCE(PLOT) = ALL
  MPCFORCES(SORT1,PLOT) = ALL
  $
  $ Event name: Event 1
  $ Event description:
  SUBCASE 1
  SUBTITLE=Event 1
  $
  $ Output Requests
  $
  STRESS(PRINT,PLOT) = ALL
  GPSTRESS(PRINT,PLOT) = ALL
  FBODYLD = ALL
  GPFORCE(PRINT,PLOT) = ALL
  $
  SPC = 1
  LOAD = 1
  BEGIN BULK
  $ HDF5 Results file
  MDLPRM,HDF5,1
  $
  $ Parts & Assemblies contained in Assembly Model_12
  $
  $
  $ Part Part_1
  $
  $ 2 3 4 5 6 7 8 9 0
  $
  $
  $ Elements for Beam Span: Span 1
  CBEAM 17 170 27 30 0. -6.12-14-1000. BOO +
  + 0. -7.5 0. 0. -7.5 0.
  CBEAM 18 170 30 29 0. -6.12-14-1000. BOO +
  + 0. -7.5 0. 0. -7.5 0.
  CBEAM 19 170 29 28 0. -6.12-14-1000. BOO +
  + 0. -7.5 0. 0. -7.5 0.
  CBEAM 20 170 28 26 0. -6.12-14-1000. BOO +
  + 0. -7.5 0. 0. -7.5 0.
  CQUAD4 9 169 21 26 28 22
  CQUAD4 10 169 22 28 29 23
  CQUAD4 11 169 23 29 30 24
  CQUAD4 12 169 24 30 27 25
  CQUAD4 13 169 26 19 18 28
  CQUAD4 14 169 28 18 17 29
  CQUAD4 15 169 29 17 16 30
  CQUAD4 16 169 30 16 20 27
  GRID 16 25. 0. 0.
  GRID 17 50.005 0. 0.
  GRID 18 75.01 0. 0.
  GRID 19 100. 0. 0.
  GRID 20 0. 0. 0.
  GRID 21 100. 50. 0.
  GRID 22 75. 50. 0.
  GRID 23 49.995 50. 0.
  GRID 24 24.99 50. 0.
  GRID 25 0. 50. 0.
  GRID 26 100. 25. 0.
  GRID 27 0. 25. 0.
  GRID 28 75. 25. 0.
  GRID 29 49.995 25. 0.
  GRID 30 24.99 25. 0.
  $ Material Record: mm
  MAT1 1 70000. .33 2.7-9
  $ Elements and Element Properties for Section: Span_1
  $ Beam properties of Beam Span: Span 1
  PBEAML 170 1 I1 +
  + 9. 1. 13. 15.
  $ Elements and Element Properties for: 2D_Element_Property_3
  PSHELL 169 1 1. 1 1
  $
  $ 2 3 4 5 6 7 8 9 0
  $
  $
  $ Static Force: Force 3
  FORCE 1 26 1. -1000.
  $ Single-Point Constraint, Alternate Form: Constraint 2
  SPC1 1 123456 20 25 27
  $
  $ 2 3 4 5 6 7 8 9 0
  $
  $
  BCPARA 0 METHOD SEGTOSEGNLGLUE 0
  ENDDATA
  
  here is the F06 result filethat you can see the GPFB results :
  
  1
  
  Warning: This computer program is protected by copyright law and international treaties.
  Unauthorized use, reproduction or distribution of this computer program, or any portion of it, may
  result in severe civil and criminal penalties.
  Copyright (C) 2025 Hexagon AB and/or its subsidiaries. All rights reserved.
  
  * * * * * * * * * * * * * * * * * * * *
  * * * * * * * * * * * * * * * * * * * *
  * * * *
  * * Hexagon AB * *
  * * * *
  * * * *
  * * M S C N a s t r a n * *
  * * * *
  * * * *
  * * * *
  * * Version 2025.1-d8fce9fe * *
  * * * *
  * * * *
  * * * *
  * * JUN 9, 2025 * *
  * * * *
  * * Intel * *
  * *MODEL 13th Gen Intel(R) Core(TM) * *
  * * Windows 10.0 19045 * *
  * * Compiled for 8664 * *
  * * * *
  * * * * * * * * * * * * * * * * * * * *
  * * * * * * * * * * * * * * * * * * * *
  1News file
  
  Welcome to MSC Nastran 2025.1
  
  MSC Nastran brings powerful new features and enhancements for engineering
  solutions in several releases through the year. Key enhancements in
  Version 2025.1 are summarized below. Addtional details can be found in
  the MSC Nastran Version 2025.1 Release Guide.
  
  MSC Nastran 2025.1 Features and Enhancements
  
  High Performance Computing (HPC)
  - Significant performance improvements for FASTFR with GPGPU acceleration
  - Significant performance improvements for acoustic panel participation
  factor calculations
  - FASTFR now enabled for models with frequency dependent properties
  - MUMPS linear solver used to accelerate residual vector computation
  for non-ACMS modal analysis
  
  SOL 200 NEO Topology Optimization
  - New convergence / Progression control for Emendate optimizer
  - Support of frequency/eigenvalue constraints for optimization
  - Support of mode tracking for normal mode optimization
  - Support of Automatic External Super Element (AESO) for normal mode
  Topology optimizations
  - New folder/file structure for a better overview of result files
  
  SOL 200 Dynamic Aero Optimization
  - SOL 200 now supports dynamic aeroelasticity (gust and frequency
  dependent loading)
  
  High Performance SOL 400 (NLPERF)
  - Support Lagrange Multiplier for MPC and Rigid Elements
  - Controls distributed surface load computation for shell elements with
  offsets and the use of an additional enhancement for computing the
  average nodal normal vector
  - GPFORCE and ESE can be requested in ANALYSIS=NLSTAT
  - OUTCTRL={STD,SOLUTION,INTERM} keyword in NLOPRM case control statement is
  available
  - The six node PENTA element is now available for use as a Gasket element
  via use of collapsed eight node CHEXA element
  - The CTRIA3/6 elements with PCOMP(G) are now available for interlaminar
  shears via collapsed CQUAD4/CQUAD8 elements
  - Support output of artificial damping energy
  - Enhancement of VCCT capability
  - Support GRAV for external modules
  
  Linear
  - In all linear solution sequencies and in SOL400 nonlinear, the solid
  composite PCOMPLS now supports the CPENTA element using a collapsed CHEXA
  1 element.
  
  Frequency Analysis
  - For frequency dependent elements at interpolated frequencies
  with only CBUSH, CELASi, CDAMPi, or CAABSF type elements
  frequency dependent, STRESS/FORCE response for these
  elements are automatically included in results.
  
  
  Adams MNF Enhancements
  - Adams MNF generation for large models has been significantly sped up.
  - MSC Nastran supports the generation of enhanced MNF files with acoustic
  modes using the uncoupled method, which facilitates the direct recovery
  of acoustic pressure in Adams. When modeling lighter fluids, the
  uncoupled method is the recommended approach.
  
  Rotordynamics
  - SOL128 analysis to start from previous converged solution. Updated
  NHRMPRM entry to read input OP2 file containing the converged solution
  from previous run and start analysis from frequency of interest.
  
  Superelements and Modules
  - MSC Nastran can now automatically generate gravity loads for external
  superelements and external modules in assembly run. This feature is
  supported for linear soutions and SOL 400 including NLPERF.
  - PLOTEL and PLTSURF are supported between modules
  through MDPLTEL and MDPLTSF respectively.
  
  Documentation
  - The complete documentation set is provided in a separate installer and
  when installed is available at: MSC_DOC_DIR/doc/pdf_nastran directory,
  where MSC_DOC_DIR is the directory where documentation was installed.
  This help set includes cross references between documents, and links to
  how-to videos, and example files
  
  Individual MSC Nastran documents are available for download from the
  Simcompanion Website at:
  http://simcompanion.hexagon.com/
  
  The documentation set includes the following:
  
  1. MSC Nastran 2025.1 Installation and Operations Guide
  2. MSC Nastran 2025.1 Quick Reference Guide
  3. MSC Nastran 2025.1 Release Guide
  4. MSC Nastran 2025.1 Linear Statics Analysis User's Guide
  5. MSC Nastran 2025.1 Dynamic Analysis User's Guide
  6. MSC Nastran 2025.1 Superelements User's Guide
  7. MSC Nastran 2025.1 Rotordynamics User's Guide
  8. MSC Nastran 2025.1 Demonstration Problems Manual
  9. MSC Nastran 2025.1 Nastran Embedded Fatigue User's Guide
  1 10. MSC Nastran 2025.1 Design Sensitivity and Optimization
  11. MSC Nastran 2025.1 Nonlinear User's Guide SOL 400
  12. MSC Nastran 2025.1 DMAP Programmer's Guide
  13. MSC Nastran 2025.1 High Performance Computing User's Guide
  14. MSC Nastran 2025.1 New Verification Manual
  15. MSC Nastran 2025.1 DEMATD Guide
  16. MSC Nastran 2025.1 Explicit Nonlinear (SOL 700) User's Guide
  17. MSC Nastran 2025.1 ACMS User's Guide
  
  Please refer to MSC_DOC_DIR/doc/pdf_nastran/nastran_library.pdf
  for the complete document set:
  
  Additional information about the release can be found at the MSC Nastran
  Product Support page: http://simcompanion.hexagon.com
  
  The support page provides links to these valuable information:
  * A searchable Knowledge Base containing examples and answers to thousands
  of frequently asked questions written by MSC Software subject-matter
  experts.
  * Peer-to-peer Discussion Forums enabling you to post questions for your
  MSC Software products and receive answers from other users worldwide.
  * A list of known issues with the product and any workarounds.
  * Instructions on how to contact technical support
  * A mechanism for sending us product feedback or enhancement requests.
  * Hardware and software requirements.
  * Examples and Tutorials
  * and much more.
  
  For information on training, please visit our Training web site
  
  https://hexagon.com/support-success/manufacturing-intelligence/
  design-engineering-support/training-materials
  
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 1
  
  0 N A S T R A N F I L E A N D S Y S T E M P A R A M E T E R E C H O
  0
  
  
  $ SYSFIELD=SCR*(RAW=YES,BUFFIO=YES,WNUM=16,WSIZE=16MB) $(C:/PROGRAM FILES/MSC.SO
  $ SYSFIELD=DBALL(RAW=YES,BUFFIO=YES,WNUM=16,WSIZE=16MB) $(C:/PROGRAM FILES/MSC.S
  NASTRAN BUFFSIZE=65537 $(C:/PROGRAM FILES/MSC.SOFTWARE/MSC_NASTRAN/2025.1/CONF/N
  $
  $
  $ $ CREATED BY MSC APEX VERSION 2024.2 ON FEB 13, 2026 AT 19:19:12
  $
  $ VALUES EXPORTED IN THIS FILE ARE EXPRESSED USING THE CONSISTENT SI_MM_T_DEG
  $ UNIT SYSTEM
  $ LENGTH MM
  $ MASS T
  $ TIME S
  $ FORCE N
  $ TEMPERATURE K
  $ NOTE: NASTRAN REQUIRES THE FOLLOWING ANGLE VALUES ALWAYS BE DEFINED IN
  $ DEGREES, WHILE ALL OTHER ROTATIONAL QUANTITIES WILL BE DEFINED IN TERMS OF
  $ RADIANS
  $ PCOMPG (THETAI - PLY ORIENTATION ANGLE)
  $ TABLED1 (YI - PHASE ANGLE DATA WHEN REFERENCED IN TP FIELD OF RLOAD2)
  $
  $ LINEAR STATIC SCENARIO STATIC SCENARIO MODEL ASSEMBLY
  $ SCENARIO DESCRIPTION
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 2
  
  0 N A S T R A N E X E C U T I V E C O N T R O L E C H O
  0
  
  
  SOL 101
  CEND
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 3
  
  0
  0 C A S E C O N T R O L E C H O
  COMMAND
  COUNT
  1 PARAM,AUTOMSET,AUTO
  2 $ AUTOMATIC STIFFNESS SINGULARITY CONSTRAINTS
  3 AUTOSPC(NOPRINT) = YES
  4 ECHO=NONE
  5 $
  6 $ OUTPUT REQUESTS
  7 $
  8 DISPLACEMENT(PLOT) = ALL
  9 STRESS(PLOT,VONMISES,CORNER) = ALL
  10 OLOAD(PLOT) = ALL
  11 SPCFORCES(PLOT) = ALL
  12 GPFORCE(PLOT) = ALL
  13 MPCFORCES(SORT1,PLOT) = ALL
  14 $
  15 $ EVENT NAME: EVENT 1
  16 $ EVENT DESCRIPTION:
  17 SUBCASE 1
  18 SUBTITLE=EVENT 1
  19 $
  20 $ OUTPUT REQUESTS
  21 $
  22 STRESS(PRINT,PLOT) = ALL
  23 GPSTRESS(PRINT,PLOT) = ALL
  24 FBODYLD = ALL
  25 GPFORCE(PRINT,PLOT) = ALL
  26 $
  27 SPC = 1
  28 LOAD = 1
  29 BEGIN BULK
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 4
  
  0
  M O D E L S U M M A R Y BULK = 0
  ENTRY NAME NUMBER OF ENTRIES
  ---------- -----------------
  BCPARA 1
  CBEAM 4
  CQUAD4 8
  FORCE 1
  GRID 15
  MAT1 1
  MDLPRM 1
  PBEAML 1
  PSHELL 1
  SPC1 1
  ^^^
  ^^^ >>> IFP OPERATIONS COMPLETE <<<
  ^^^
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK CASECC, TRAILER[102, 1, 0, 1013, 0, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM1Q, TRAILER[101, 0, 0, 8, 0, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK EPT, TRAILER[101, 0, 512, 0, 1024, 0, 16])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK MPT, TRAILER[102, 32768, 0, 0, 0, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM2, TRAILER[103, 0, 0, 0, 9216, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM3S, TRAILER[104, 0, 0, 64, 0, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (DATA BLOCK GEOM3S IS NOT SUPPORTED)
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM4S, TRAILER[105, 0, 0, 0, 64, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (DATA BLOCK GEOM4S IS NOT SUPPORTED)
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM1, TRAILER[101, 0, 0, 8, 0, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK EDT, TRAILER[103, 0, 0, 0, 0, 0, 4])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM3, TRAILER[101, 0, 0, 64, 0, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM4, TRAILER[102, 0, 0, 0, 64, 0, 0])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK CONTACT, TRAILER[101, 32, 0, 0, 0, 0, 0])
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 5
  
  0
  *** USER INFORMATION MESSAGE 7310 (VECPRN)
  ORIGIN OF SUPERELEMENT OR MODULE BASIC COORDINATE SYSTEM WILL BE USED AS REFERENCE LOCATION.
  RESULTANTS ABOUT ORIGIN OF SUPERELEMENT OR MODULE BASIC COORDINATE SYSTEM IN SUPERELEMENT OR MODULE
  BASIC SYSTEM COORDINATES.
  0 OLOAD RESULTANT
  SUBCASE/ LOAD
  DAREA ID TYPE T1 T2 T3 R1 R2 R3
  0 1 FX 0.000000E+00 ---- ---- ---- 0.000000E+00 0.000000E+00
  FY ---- 0.000000E+00 ---- 0.000000E+00 ---- 0.000000E+00
  FZ ---- ---- -1.000000E+03 -2.500000E+04 1.000000E+05 ----
  MX ---- ---- ---- 0.000000E+00 ---- ----
  MY ---- ---- ---- ---- 0.000000E+00 ----
  MZ ---- ---- ---- ---- ---- 0.000000E+00
  TOTALS 0.000000E+00 0.000000E+00 -1.000000E+03 -2.500000E+04 1.000000E+05 0.000000E+00
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 6
  
  0 SUBCASE 1
  
  *** SYSTEM INFORMATION MESSAGE 4159 (DFMSA)
  THE DECOMPOSITION OF KLL YIELDS A MAXIMUM MATRIX-TO-FACTOR-DIAGONAL RATIO OF 1.127789E+01
  ^^^
  *** USER INFORMATION MESSAGE 15201 (SUBDMAP SEKRRS)
  Condition number of stiffness matrix = 1.960347E+06
  ^^^
  *** USER INFORMATION MESSAGE 5293 (SSG3B)
  FOR DATA BLOCK KLL
  LOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
  1 -6.0429181E-15 1.2152427E+03
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 7
  
  0
  *** USER INFORMATION MESSAGE 7310 (VECPRN)
  ORIGIN OF SUPERELEMENT OR MODULE BASIC COORDINATE SYSTEM WILL BE USED AS REFERENCE LOCATION.
  RESULTANTS ABOUT ORIGIN OF SUPERELEMENT OR MODULE BASIC COORDINATE SYSTEM IN SUPERELEMENT OR MODULE
  BASIC SYSTEM COORDINATES.
  0 SPCFORCE RESULTANT
  SUBCASE/ LOAD
  DAREA ID TYPE T1 T2 T3 R1 R2 R3
  0 1 FX 1.409717E-11 ---- ---- ---- 0.000000E+00 2.840434E-01
  FY ---- -5.684342E-13 ---- 0.000000E+00 ---- 0.000000E+00
  FZ ---- ---- 1.000000E+03 2.499999E+04 0.000000E+00 ----
  MX ---- ---- ---- 6.554775E-03 ---- ----
  MY ---- ---- ---- ---- -1.000000E+05 ----
  MZ ---- ---- ---- ---- ---- -2.840434E-01
  TOTALS 1.409717E-11 -5.684342E-13 1.000000E+03 2.500000E+04 -1.000000E+05 -5.135807E-10
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 8
  
  0
  *** USER INFORMATION MESSAGE 7310 (VECPRN)
  ORIGIN OF SUPERELEMENT OR MODULE BASIC COORDINATE SYSTEM WILL BE USED AS REFERENCE LOCATION.
  RESULTANTS ABOUT ORIGIN OF SUPERELEMENT OR MODULE BASIC COORDINATE SYSTEM IN SUPERELEMENT OR MODULE
  BASIC SYSTEM COORDINATES.
  0 MPCFORCE RESULTANT
  SUBCASE/ LOAD
  DAREA ID TYPE T1 T2 T3 R1 R2 R3
  0 1 FX 0.000000E+00 ---- ---- ---- 0.000000E+00 0.000000E+00
  FY ---- 0.000000E+00 ---- 0.000000E+00 ---- 0.000000E+00
  FZ ---- ---- 0.000000E+00 0.000000E+00 0.000000E+00 ----
  MX ---- ---- ---- 0.000000E+00 ---- ----
  MY ---- ---- ---- ---- 0.000000E+00 ----
  MZ ---- ---- ---- ---- ---- 0.000000E+00
  TOTALS 0.000000E+00 0.000000E+00 0.000000E+00 0.000000E+00 0.000000E+00 0.000000E+00
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 9
  EVENT 1
  0 SUBCASE 1
  
  S T R E S S E S I N B E A M E L E M E N T S ( C B E A M )
  STAT DIST/
  ELEMENT-ID GRID LENGTH SXC SXD SXE SXF S-MAX S-MIN M.S.-T M.S.-C
  0 17
  27 0.000 -2.033890E+02 5.410170E+02 5.410131E+02 -2.033930E+02 5.410170E+02 -2.033930E+02
  30 1.000 -4.560338E+01 3.832336E+02 3.832274E+02 -4.560953E+01 3.832336E+02 -4.560953E+01
  0 18
  30 0.000 -1.663895E+02 4.086462E+02 4.086459E+02 -1.663898E+02 4.086462E+02 -1.663898E+02
  29 1.000 -8.559467E+00 2.508200E+02 2.508159E+02 -8.563648E+00 2.508200E+02 -8.563648E+00
  0 19
  29 0.000 -1.301140E+02 2.765243E+02 2.765259E+02 -1.301124E+02 2.765259E+02 -1.301140E+02
  28 1.000 2.771832E+01 1.186978E+02 1.186936E+02 2.771411E+01 1.186978E+02 2.771411E+01
  0 20
  28 0.000 -9.577726E+01 1.447575E+02 1.447591E+02 -9.577559E+01 1.447591E+02 -9.577726E+01
  26 1.000 6.204381E+01 -1.305900E+01 -1.306195E+01 6.204086E+01 6.204381E+01 -1.306195E+01
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 10
  EVENT 1
  0 SUBCASE 1
  
  S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 ) OPTION = BILIN
  
  ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)
  ID GRID-ID DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
  0 9 CEN/4 -5.000000E-01 -1.136696E+01 -1.429658E+01 1.515733E+01 42.2400 2.396175E+00 -2.805972E+01 2.933130E+01
  5.000000E-01 -6.843047E+00 -1.803396E+01 1.469982E+01 34.5804 3.290260E+00 -2.816726E+01 2.994826E+01
  21 -5.000000E-01 -2.888758E+01 -1.073200E+01 1.515733E+01 60.4588 -2.141996E+00 -3.747758E+01 3.645381E+01
  5.000000E-01 -2.426236E+01 -1.418525E+01 1.469982E+01 54.4599 -3.684441E+00 -3.476317E+01 3.307522E+01
  26 -5.000000E-01 -2.888758E+01 -1.786116E+01 1.515733E+01 54.9940 -7.245508E+00 -3.950323E+01 3.642501E+01
  5.000000E-01 -2.426236E+01 -2.188266E+01 1.469982E+01 47.3138 -8.324614E+00 -3.782041E+01 3.442154E+01
  28 -5.000000E-01 6.153654E+00 -1.786116E+01 1.515733E+01 25.8071 1.348332E+01 -2.519083E+01 3.400050E+01
  5.000000E-01 1.057627E+01 -2.188266E+01 1.469982E+01 21.0843 1.624384E+01 -2.755024E+01 3.834579E+01
  22 -5.000000E-01 6.153654E+00 -1.073200E+01 1.515733E+01 30.4408 1.506093E+01 -1.963927E+01 3.013832E+01
  5.000000E-01 1.057627E+01 -1.418525E+01 1.469982E+01 24.9473 1.741446E+01 -2.102344E+01 3.333707E+01
  0 10 CEN/4 -5.000000E-01 1.047673E+00 -4.064693E+01 1.833570E+01 20.6662 7.963797E+00 -4.756306E+01 5.200432E+01
  5.000000E-01 2.724596E+00 -5.598804E+01 1.706542E+01 15.0852 7.324455E+00 -6.058790E+01 6.456248E+01
  22 -5.000000E-01 -2.541963E+00 -3.873408E+01 1.833570E+01 22.6884 5.123679E+00 -4.639972E+01 4.916222E+01
  5.000000E-01 -1.948576E+00 -5.338241E+01 1.706542E+01 16.7839 3.198538E+00 -5.852953E+01 6.019257E+01
  28 -5.000000E-01 -2.541963E+00 -4.255979E+01 1.833570E+01 21.2507 4.588662E+00 -4.969041E+01 5.213641E+01
  5.000000E-01 -1.948576E+00 -5.859366E+01 1.706542E+01 15.5353 2.795405E+00 -6.333764E+01 6.478060E+01
  29 -5.000000E-01 4.637308E+00 -4.255979E+01 1.833570E+01 18.9233 1.092336E+01 -4.884584E+01 5.512528E+01
  5.000000E-01 7.397768E+00 -5.859366E+01 1.706542E+01 13.6740 1.154967E+01 -6.274557E+01 6.924660E+01
  23 -5.000000E-01 4.637308E+00 -3.873408E+01 1.833570E+01 20.1076 1.134998E+01 -4.544675E+01 5.205813E+01
  5.000000E-01 7.397768E+00 -5.338241E+01 1.706542E+01 14.6581 1.186146E+01 -5.784611E+01 6.459880E+01
  0 11 CEN/4 -5.000000E-01 6.590103E+00 -6.411282E+01 1.258061E+01 9.7946 8.761935E+00 -6.628465E+01 7.107185E+01
  5.000000E-01 3.061383E+00 -9.577869E+01 1.280617E+01 7.2637 4.693653E+00 -9.741096E+01 9.984056E+01
  23 -5.000000E-01 -3.106433E+00 -5.683060E+01 1.258061E+01 12.5478 -3.063654E-01 -5.963067E+01 5.947808E+01
  5.000000E-01 -5.733147E+00 -9.118402E+01 1.280617E+01 8.3426 -3.855211E+00 -9.306196E+01 9.119549E+01
  29 -5.000000E-01 -3.106433E+00 -7.139503E+01 1.258061E+01 10.1133 -8.624808E-01 -7.363899E+01 7.321156E+01
  5.000000E-01 -5.733147E+00 -1.003734E+02 1.280617E+01 7.5716 -4.030907E+00 -1.020756E+02 1.001210E+02
  30 -5.000000E-01 1.628664E+01 -7.139503E+01 1.258061E+01 8.0057 1.805601E+01 -7.316440E+01 8.366664E+01
  5.000000E-01 1.185591E+01 -1.003734E+02 1.280617E+01 6.4278 1.329864E+01 -1.018161E+02 1.090751E+02
  24 -5.000000E-01 1.628664E+01 -5.683060E+01 1.258061E+01 9.4947 1.839072E+01 -5.893468E+01 6.996689E+01
  5.000000E-01 1.185591E+01 -9.118402E+01 1.280617E+01 6.9795 1.342366E+01 -9.275177E+01 1.001407E+02
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 11
  EVENT 1
  0 SUBCASE 1
  
  S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 ) OPTION = BILIN
  
  ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)
  ID GRID-ID DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
  0 12 CEN/4 -5.000000E-01 -1.120846E+01 -9.069818E+01 1.378621E+01 9.5650 -8.885363E+00 -9.302128E+01 8.891221E+01
  5.000000E-01 -2.187227E+01 -1.321325E+02 1.536674E+01 7.7875 -1.977070E+01 -1.342340E+02 1.255219E+02
  24 -5.000000E-01 7.513471E+00 -7.275135E+01 1.378621E+01 9.4793 9.815361E+00 -7.505324E+01 8.041147E+01
  5.000000E-01 -1.408336E-01 -1.129928E+02 1.536674E+01 7.6171 1.914192E+00 -1.150478E+02 1.160167E+02
  30 -5.000000E-01 7.513471E+00 -1.086450E+02 1.378621E+01 6.6766 9.127259E+00 -1.102588E+02 1.150942E+02
  5.000000E-01 -1.408336E-01 -1.512722E+02 1.536674E+01 5.7474 1.405799E+00 -1.528188E+02 1.535265E+02
  27 -5.000000E-01 -2.993040E+01 -1.086450E+02 1.378621E+01 9.6523 -2.758570E+01 -1.109897E+02 1.000897E+02
  5.000000E-01 -4.360371E+01 -1.512722E+02 1.536674E+01 7.9656 -4.145347E+01 -1.534224E+02 1.374661E+02
  25 -5.000000E-01 -2.993040E+01 -7.275135E+01 1.378621E+01 16.3887 -2.587584E+01 -7.680591E+01 6.768522E+01
  5.000000E-01 -4.360371E+01 -1.129928E+02 1.536674E+01 11.9446 -4.035293E+01 -1.162436E+02 1.022260E+02
  0 13 CEN/4 -5.000000E-01 -1.136775E+01 -1.429549E+01 -1.515773E+01 -42.2419 2.396635E+00 -2.805988E+01 2.933172E+01
  5.000000E-01 -6.839453E+00 -1.803052E+01 -1.469695E+01 -34.5784 3.291115E+00 -2.816109E+01 2.994261E+01
  26 -5.000000E-01 -2.889115E+01 -1.786593E+01 -1.515562E+01 -54.9940 -7.251488E+00 -3.950559E+01 3.642529E+01
  5.000000E-01 -2.425817E+01 -2.188590E+01 -1.469482E+01 -47.3074 -8.329420E+00 -3.781465E+01 3.441443E+01
  19 -5.000000E-01 -2.889816E+01 -1.072458E+01 -1.515634E+01 -60.4721 -2.139804E+00 -3.748294E+01 3.646016E+01
  5.000000E-01 -2.426514E+01 -1.417463E+01 -1.469559E+01 -54.4741 -3.682348E+00 -3.475742E+01 3.307036E+01
  18 -5.000000E-01 6.162665E+00 -1.072458E+01 -1.515984E+01 -30.4417 1.507172E+01 -1.963364E+01 3.014216E+01
  5.000000E-01 1.058623E+01 -1.417463E+01 -1.469908E+01 -24.9470 1.742397E+01 -2.101237E+01 3.333516E+01
  28 -5.000000E-01 6.155653E+00 -1.786593E+01 -1.515913E+01 -25.8049 1.348545E+01 -2.519572E+01 3.400673E+01
  5.000000E-01 1.057926E+01 -2.188590E+01 -1.469831E+01 -21.0801 1.624501E+01 -2.755165E+01 3.834802E+01
  0 14 CEN/4 -5.000000E-01 1.053332E+00 -4.064607E+01 -1.832976E+01 -20.6600 7.964939E+00 -4.755768E+01 5.199968E+01
  5.000000E-01 2.730238E+00 -5.598267E+01 -1.705311E+01 -15.0761 7.323892E+00 -6.057632E+01 6.455064E+01
  28 -5.000000E-01 -2.534905E+00 -4.256767E+01 -1.832866E+01 -21.2399 4.589002E+00 -4.969158E+01 5.213777E+01
  5.000000E-01 -1.939581E+00 -5.860087E+01 -1.705165E+01 -15.5214 2.796134E+00 -6.333659E+01 6.477993E+01
  18 -5.000000E-01 -2.534905E+00 -3.872448E+01 -1.832943E+01 -22.6845 5.126652E+00 -4.638604E+01 4.915030E+01
  5.000000E-01 -1.939580E+00 -5.336447E+01 -1.705270E+01 -16.7763 3.201245E+00 -5.850529E+01 6.016982E+01
  17 -5.000000E-01 4.641570E+00 -3.872448E+01 -1.833086E+01 -20.1056 1.135175E+01 -4.543466E+01 5.204742E+01
  5.000000E-01 7.400057E+00 -5.336447E+01 -1.705456E+01 -14.6535 1.185944E+01 -5.782385E+01 6.457555E+01
  29 -5.000000E-01 4.641570E+00 -4.256767E+01 -1.833010E+01 -18.9155 1.092291E+01 -4.884901E+01 5.512811E+01
  5.000000E-01 7.400056E+00 -5.860087E+01 -1.705352E+01 -13.6642 1.154597E+01 -6.274678E+01 6.924551E+01
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 12
  EVENT 1
  0 SUBCASE 1
  
  S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 ) OPTION = BILIN
  
  ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)
  ID GRID-ID DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
  0 15 CEN/4 -5.000000E-01 6.598697E+00 -6.411162E+01 -1.257020E+01 -9.7862 8.766826E+00 -6.627975E+01 7.106986E+01
  5.000000E-01 3.069155E+00 -9.577531E+01 -1.278675E+01 -7.2529 4.696487E+00 -9.740264E+01 9.983377E+01
  29 -5.000000E-01 -3.098994E+00 -7.139889E+01 -1.256680E+01 -10.1015 -8.601604E-01 -7.363772E+01 7.321143E+01
  5.000000E-01 -5.729242E+00 -1.003776E+02 -1.278407E+01 -7.5585 -4.032912E+00 -1.020739E+02 1.001184E+02
  17 -5.000000E-01 -3.098993E+00 -5.682435E+01 -1.256971E+01 -12.5380 -3.036000E-01 -5.961974E+01 5.946852E+01
  5.000000E-01 -5.729242E+00 -9.117303E+01 -1.278591E+01 -8.3308 -3.856969E+00 -9.304530E+01 9.117802E+01
  16 -5.000000E-01 1.629639E+01 -5.682435E+01 -1.257359E+01 -9.4894 1.839809E+01 -5.892605E+01 6.996353E+01
  5.000000E-01 1.186755E+01 -9.117303E+01 -1.278943E+01 -6.9707 1.343125E+01 -9.273672E+01 1.001303E+02
  30 -5.000000E-01 1.629639E+01 -7.139889E+01 -1.257068E+01 -7.9985 1.806275E+01 -7.316525E+01 8.367188E+01
  5.000000E-01 1.186755E+01 -1.003776E+02 -1.278759E+01 -6.4179 1.330595E+01 -1.018160E+02 1.090793E+02
  0 16 CEN/4 -5.000000E-01 -1.120723E+01 -9.069679E+01 -1.377724E+01 -9.5592 -8.887067E+00 -9.301696E+01 8.890718E+01
  5.000000E-01 -2.187196E+01 -1.321338E+02 -1.535293E+01 -7.7808 -1.977412E+01 -1.342317E+02 1.255183E+02
  30 -5.000000E-01 7.519140E+00 -1.086459E+02 -1.377731E+01 -6.6720 9.130787E+00 -1.102575E+02 1.150949E+02
  5.000000E-01 -1.356698E-01 -1.512736E+02 -1.535319E+01 -5.7422 1.408198E+00 -1.528175E+02 1.535264E+02
  16 -5.000000E-01 7.511650E+00 -7.275010E+01 -1.378090E+01 -9.4762 9.811900E+00 -7.505035E+01 8.040656E+01
  5.000000E-01 -1.443639E-01 -1.129966E+02 -1.535702E+01 -7.6125 1.908103E+00 -1.150491E+02 1.160149E+02
  20 -5.000000E-01 -2.992612E+01 -7.275010E+01 -1.377716E+01 -16.3793 -2.587670E+01 -7.679952E+01 6.767904E+01
  5.000000E-01 -4.359955E+01 -1.129966E+02 -1.535267E+01 -11.9337 -4.035480E+01 -1.162413E+02 1.022236E+02
  27 -5.000000E-01 -2.993361E+01 -1.086459E+02 -1.377357E+01 -9.6443 -2.759302E+01 -1.109865E+02 1.000846E+02
  5.000000E-01 -4.360825E+01 -1.512736E+02 -1.534885E+01 -7.9570 -4.146285E+01 -1.534190E+02 1.374604E+02
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 13
  EVENT 1
  0 SUBCASE 1
  
  G R I D P O I N T F O R C E B A L A N C E
  
  POINT-ID ELEMENT-ID SOURCE T1 T2 T3 R1 R2 R3
  16 15 QUAD4 -1.133279E+03 -5.974658E+01 -2.594148E-01 2.330020E+00 4.394660E+01 3.462614E-01
  16 16 QUAD4 1.133279E+03 5.974658E+01 2.594148E-01 -2.330020E+00 -4.394660E+01 -3.462614E-01
  16 *TOTALS* -9.094947E-13 2.131628E-14 4.973799E-14 -2.740030E-13 -2.273737E-13 5.551115E-16
  0 17 14 QUAD4 -8.158016E+02 -1.804920E+02 -3.335592E-01 8.758080E+00 2.388863E+01 -6.018500E-02
  17 15 QUAD4 8.158016E+02 1.804920E+02 3.335592E-01 -8.758080E+00 -2.388863E+01 6.018500E-02
  17 *TOTALS* -2.273737E-13 -2.842171E-13 -3.552714E-13 -1.289635E-12 -1.250555E-12 -1.665335E-16
  0 18 13 QUAD4 -3.731566E+02 -2.276192E+02 -2.310961E-01 6.543553E+00 7.583922E+00 1.567281E-01
  18 14 QUAD4 3.731566E+02 2.276192E+02 2.310961E-01 -6.543553E+00 -7.583922E+00 -1.567281E-01
  18 *TOTALS* 3.410605E-13 -1.421085E-13 5.115908E-13 4.247269E-12 1.136868E-12 -5.551115E-16
  0 19 13 QUAD4 4.964362E-13 -5.595524E-14 -3.979039E-13 -3.709033E-12 -6.821210E-13 5.551115E-17
  19 *TOTALS* 4.964362E-13 -5.595524E-14 -3.979039E-13 -3.709033E-12 -6.821210E-13 5.551115E-17
  0 20 F-OF-SPC 1.497563E+03 4.732266E+02 1.776723E-01 1.886259E+01 -4.155103E+01 4.752403E-01
  20 16 QUAD4 -1.497563E+03 -4.732266E+02 -1.776723E-01 -1.886259E+01 4.155103E+01 -4.752403E-01
  20 *TOTALS* 0.0 0.0 -3.552714E-15 7.815970E-14 7.815970E-14 0.0
  0 21 9 QUAD4 1.139921E-12 1.145611E-13 -3.979039E-13 -1.113026E-12 2.955858E-12 1.415534E-15
  21 *TOTALS* 1.139921E-12 1.145611E-13 -3.979039E-13 -1.113026E-12 2.955858E-12 1.415534E-15
  0 22 9 QUAD4 -3.732444E+02 2.276251E+02 -2.309971E-01 -6.537360E+00 7.588891E+00 -1.567309E-01
  22 10 QUAD4 3.732444E+02 -2.276251E+02 2.309971E-01 6.537360E+00 -7.588891E+00 1.567309E-01
  22 *TOTALS* -3.979039E-13 -3.126388E-13 1.236344E-12 9.050538E-13 2.046363E-12 -1.665335E-16
  0 23 10 QUAD4 -8.158666E+02 1.804623E+02 -3.333359E-01 -8.752412E+00 2.389065E+01 6.012049E-02
  23 11 QUAD4 8.158666E+02 -1.804623E+02 3.333359E-01 8.752412E+00 -2.389065E+01 -6.012049E-02
  23 *TOTALS* 5.684342E-13 2.842171E-13 -5.329071E-13 2.861711E-12 2.614797E-12 8.326673E-16
  0 24 11 QUAD4 -1.133293E+03 5.979460E+01 -2.591261E-01 -2.327065E+00 4.394627E+01 -3.463173E-01
  24 12 QUAD4 1.133293E+03 -5.979460E+01 2.591261E-01 2.327065E+00 -4.394627E+01 3.463173E-01
  24 *TOTALS* 2.273737E-13 -1.421085E-14 4.263256E-14 -2.637890E-13 1.477929E-12 5.551115E-17
  0 25 F-OF-SPC 1.497551E+03 -4.731384E+02 1.774101E-01 -1.885887E+01 -4.154679E+01 -4.752839E-01
  25 12 QUAD4 -1.497551E+03 4.731384E+02 -1.774101E-01 1.885887E+01 4.154679E+01 4.752839E-01
  25 *TOTALS* -2.273737E-13 -5.684342E-14 -2.842171E-14 1.314504E-13 1.136868E-13 0.0
  0 26 APP-LOAD 0.0 0.0 -1.000000E+03 0.0 0.0 0.0
  26 20 BEAM -8.082007E+02 -3.097485E-03 9.803701E+02 9.786219E-03 -2.298041E+02 -1.338929E-03
  26 9 QUAD4 4.041317E+02 -3.731844E+02 9.814060E+00 9.495169E+00 1.148896E+02 -7.146908E-01
  26 13 QUAD4 4.040690E+02 3.731875E+02 9.815803E+00 -9.504955E+00 1.149146E+02 7.160298E-01
  26 *TOTALS* -3.012701E-12 -5.684342E-14 -6.068035E-12 1.264766E-12 3.055334E-11 1.986189E-13
  0 27 F-OF-SPC -2.995114E+03 -8.820442E-02 9.996449E+02 2.836065E-03 -9.991690E+04 -2.839998E-01
  27 17 BEAM 5.570797E+03 1.485998E-03 -9.805499E+02 -6.405167E-03 9.958432E+04 2.839343E-01
  27 12 QUAD4 -1.287832E+03 -1.087188E+02 -9.548477E+00 -5.437613E+00 1.662996E+02 3.276885E-05
  27 16 QUAD4 -1.287851E+03 1.088056E+02 -9.546539E+00 5.441182E+00 1.662792E+02 3.276885E-05
  27 *TOTALS* -6.821210E-13 1.421085E-14 -2.771117E-13 -1.527667E-13 2.046363E-12 -5.278709E-18
  0 28 19 BEAM -2.415797E+03 -3.914443E-03 9.802404E+02 1.724897E-02 -2.518313E+04 -8.123905E-02
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 14
  EVENT 1
  0 SUBCASE 1
  
  G R I D P O I N T F O R C E B A L A N C E
  
  POINT-ID ELEMENT-ID SOURCE T1 T2 T3 R1 R2 R3
  28 20 BEAM 8.082007E+02 3.097485E-03 -9.803701E+02 -9.786219E-03 2.473906E+04 7.877605E-02
  28 9 QUAD4 -3.088730E+01 1.455593E+02 -9.583063E+00 2.817117E+00 1.228731E+02 -6.276362E-01
  28 10 QUAD4 8.346927E+02 -2.148692E+02 9.648767E+00 9.279042E+00 9.915000E+01 -6.277568E-01
  28 13 QUAD4 -3.091246E+01 -1.455684E+02 -9.584707E+00 -2.816002E+00 1.228943E+02 6.287820E-01
  28 14 QUAD4 8.347028E+02 2.148790E+02 9.648770E+00 -9.287620E+00 9.915044E+01 6.290740E-01
  28 *TOTALS* 4.661160E-12 -5.968559E-13 -3.154810E-12 1.566747E-12 -4.820322E-11 -2.182698E-13
  0 29 18 BEAM -3.997231E+03 -2.579057E-03 9.802321E+02 1.313726E-02 -5.012020E+04 -1.809647E-01
  29 19 BEAM 2.415797E+03 3.914443E-03 -9.802404E+02 -1.724897E-02 4.969404E+04 1.791197E-01
  29 10 QUAD4 -3.920705E+02 2.620320E+02 -9.546428E+00 -4.505518E+00 1.315917E+02 -5.747276E-01
  29 11 QUAD4 1.182777E+03 -1.368441E+02 9.550621E+00 2.025961E+00 8.149426E+01 -5.748057E-01
  29 14 QUAD4 -3.920578E+02 -2.620062E+02 -9.546307E+00 4.511517E+00 1.315899E+02 5.756430E-01
  29 15 QUAD4 1.182785E+03 1.368169E+02 9.550432E+00 -2.027848E+00 8.149269E+01 5.757353E-01
  29 *TOTALS* 1.705303E-11 -2.557954E-13 -9.450218E-13 -1.830536E-12 2.092975E-10 -5.366818E-13
  0 30 17 BEAM -5.570797E+03 -1.485998E-03 9.805499E+02 6.405167E-03 -7.508038E+04 -2.467992E-01
  30 18 BEAM 3.997231E+03 2.579057E-03 -9.802321E+02 -1.313726E-02 7.463091E+04 2.454540E-01
  30 11 QUAD4 -8.653507E+02 2.575118E+02 -9.624831E+00 -1.030655E+01 1.455985E+02 -4.353516E-01
  30 12 QUAD4 1.652090E+03 -3.046250E+02 9.466761E+00 -1.779122E+01 7.914979E+01 -4.350198E-01
  30 15 QUAD4 -8.653077E+02 -2.575624E+02 -9.624576E+00 1.030952E+01 1.455993E+02 4.358667E-01
  30 16 QUAD4 1.652134E+03 3.046745E+02 9.464796E+00 1.779499E+01 7.912705E+01 4.358499E-01
  30 *TOTALS* -1.591616E-12 6.821210E-13 3.517187E-12 -2.160050E-12 -1.130616E-10 -7.102652E-13
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK OUG1, TRAILER[101, 0, 120, 0, 0, 0, 2])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK OES1X, TRAILER[101, 63, 2, 13, 26, 0, 3])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK OGPFB1, TRAILER[101, 0, 1, 0, 0, 0, 3])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK OPG1, TRAILER[101, 0, 120, 0, 0, 0, 2])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK OQG1, TRAILER[102, 0, 120, 0, 0, 0, 2])
  *** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
  *** USER INFORMATION MESSAGE (WRITE DATA BLOCK OQMG1, TRAILER[104, 0, 120, 0, 0, 0, 2])
  1 FEBRUARY 13, 2026 MSC Nastran 6/ 9/25 PAGE 15
  
  0
  * * * * D B D I C T P R I N T * * * * SUBDMAP = PRTSUM , DMAP STATEMENT NO. 75
  
  0 * * * * A N A L Y S I S S U M M A R Y T A B L E * * * *
  0 SEID PEID PROJ VERS APRCH SEMG SEMR SEKR SELG SELR MODES DYNRED SOLLIN SOLNL LOOPID DESIGN CYCLE SENSITIVITY
  -------------------------------------------------------------------------------------------------------------------
  0 0 1 1 ' ' T T T T T F F T F -1 0 F
  0SEID = SUPERELEMENT ID.
  PEID = PRIMARY SUPERELEMENT ID OF IMAGE SUPERELEMENT.
  PROJ = PROJECT ID NUMBER.
  VERS = VERSION ID.
  APRCH = BLANK FOR STRUCTURAL ANALYSIS. HEAT FOR HEAT TRANSFER ANALYSIS.
  SEMG = STIFFNESS AND MASS MATRIX GENERATION STEP.
  SEMR = MASS MATRIX REDUCTION STEP (INCLUDES EIGENVALUE SOLUTION FOR MODES).
  SEKR = STIFFNESS MATRIX REDUCTION STEP.
  SELG = LOAD MATRIX GENERATION STEP.
  SELR = LOAD MATRIX REDUCTION STEP.
  MODES = T (TRUE) IF NORMAL MODES OR BUCKLING MODES CALCULATED.
  DYNRED = T (TRUE) MEANS GENERALIZED DYNAMIC AND/OR COMPONENT MODE REDUCTION PERFORMED.
  SOLLIN = T (TRUE) IF LINEAR SOLUTION EXISTS IN DATABASE.
  LOOPID = THE LAST LOOPID VALUE USED IN THE NONLINEAR ANALYSIS. USEFUL FOR RESTARTS.
  SOLNL = T (TRUE) IF NONLINEAR SOLUTION EXISTS IN DATABASE.
  DESIGN CYCLE = THE LAST DESIGN CYCLE (ONLY VALID IN OPTIMIZATION).
  SENSITIVITY = SENSITIVITY MATRIX GENERATION FLAG.
  
  No PARAM values were set in the Control File.
  
  1 * * * END OF JOB * * *
  
  No Symbolic Replacement variables or values were specified.
  
  we are dealing with "FREEBODY LOADS".
- February 19, 2026 at 8:34 am
  
  e195027
  Subscriber
  
  I don't think ANSYS has the capability for free body load extraction.

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