Non-linear Frame Analysis

Another example using Fortran code published in Programming the Finite Element Method (5th ed. John Wiley & Sons, I.M. Smith, D.V. Griffiths and L. Margetts (2014)), this post provides a spreadsheet based frame analysis program including non-linear bending behaviour and 2D or 3D analysis, linking to Fortran solver functions, via Python and xlwings.  Note that at present the spreadsheet has only rudimentary functionality for post-processing and plotting of results, and only provides input for loads at nodes, so for linear analysis the spreadsheets Frame4 and 3DFrame provide better functionality.

The new spreadsheet and related files, including full open source code, may be downloaded from:

To run the spreadsheet, in addition to Excel, the requirements are:

  • Python, including Numpy, Scipy and Ctypes
  • Xlwings
  • The provided compiled Fortran files, Main.dll and Geom.dll may be installed anywhere on the system path, or in the same directory as the spreadsheet and Python files.

The simplest way to install the required Python modules is to install Anaconda Python, which includes xlwings.  The program has been tested with Python 2.7.  It should work with Python 3, but if not, please let me know.

The program is based on Program P45 from Edition 5 of Programming the Finite element Method.  The beam elements are treated as elastic – perfectly plastic, and specified nodal loads may be factored in any number of load increments.  The download file includes data for the 3D frame analysis shown below:


Data is input on the spreadsheet, with any number of material types, nodes and beam elements (up to the 1 million+ rows provided by Excel):


Forces and moments are applied at nodes only in the current version.  Specified loads are factored by any number of load increments:


Input for 2D analyses is in a similar format, with data restricted to the available freedoms (X and Y directions, and moments about the Z axis):


The analysis is run by clicking a button on the “Results” sheet.  Full lists of node deflections and beam end actions are copied to the “Deflect” and “StressRes” sheets respectively.  At present the “Results” sheet only provides a brief summary of each load increment, and plots of deflections for one node, and forces and moments for one beam, with up to 8 load increments.  This will be extended in later versions.


The example output also plots X deflection and Z-axis moment results from the finite element analysis program Strand7, using the same elastic-plastic beam properties.  It can be seen that there is good agreement between the two, although not exact due to different methods of modelling the non-linear behaviour.


Strand7 provides a facility to re-number nodes, to improve the efficiency of the matrix solution process.  Three different node numbering sequences have been copied to the spreadsheet, and it can be seen below (row 7) that the solution times for this medium sized frame are almost unchanged.  For a larger frame (2730 Nodes and 7065 beams) the “tree” node sequence was about four times faster than the other two options.


This entry was posted in Beam Bending, Excel, Finite Element Analysis, Fortran, Frame Analysis, Link to dll, Link to Python, Newton, NumPy and SciPy, Strand7, UDFs, VBA and tagged , , , , , , , , , , . Bookmark the permalink.

3 Responses to Non-linear Frame Analysis

  1. Bill harvey says:

    Not a job for you I know, but surely it is time these solvers were recoded using the amazing matrix handling of python?


    • dougaj4 says:

      Hi Bill, actually that’s part of the plan.
      The previous spreadsheets posted in the recent series used Python purely as a link from Excel to the Fortran. In this one the top level code has been translated to Python, calling the Fortran subroutines for the maths intensive bits. The next stage is to try the Scipy sparse matrix solvers, which I’m hoping will give much better performance with very big models.


  2. Pingback: Non-linear Frame Analysis – Scipy solvers | Newton Excel Bach, not (just) an Excel Blog

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