The parameters “camber_relaxation”, “le_loc”, and “camber_termination_tol” then Run to determine the camber line and thickness distribution of the airfoil. Points, then when this class is initialized, a solver will be automatically If the airfoil geometry is defined using outline Airfoil ( name, airfoil_input, **kwargs ) ¶Ī class defining an airfoil. The following member functions are available: class airfoil_db. For an example of using the Airfoil class to generate and export a database, see the examples/ directory. The Airfoil class can create geometries, create a database using Xfoil, export and import databases, curve fit a database, import and export curve fits, and calculate section properties.
All functionality is wrapped in the Airfoil class.
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