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Using Abaqus Script to Generate Airfoil Section and Interior Stucture

Oct 18, 2016, NUAA

  • Code was write by Python 3.4 using Anaconda, but can also work under Python 2.7 interpreter.

  • The module SectionBuilderSubroutine.pyc used in the main program AbaqusAirfoilSectionBuilder.py shall be placed in the Abaqus working path, for example,

    'F:\User\Documents\Work\Abaqus', in order to work properly. The path can be set in the GUI mode by clicking File->Set Work Directory .

  • In the main script AbaqusAirfoilSectionBuilder.py, replace the input_file parameter with the full path of your input file, usually the airfoil data file.

  • The input_file (airfoil data) should be a close curve points set.

  • The control point D which be used to decide the position of the C-beam, shalled by modifed for airfoil with high curvature.

  • For more information, contact the author at [email protected]

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