:orphan:

.. _geometry_2_child:

geometry_child
==============

.. autoclass:: ansys.fluent.core.generated.solver.settings_251.geometry_2_child
    :show-inheritance:

.. rubric:: Attributes

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Attribute                                                                                                                                     Summary

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:ref:`name <name_5>`                                                                                                        Specify the section name.

:ref:`radius_ratio <radius_ratio>`                 Specify the span-wise distance of the blade section from rotor origin over rotor tip radius (r/R).

:ref:`chord <chord>`                                                                                       Specify the chord lenght at blade section.

:ref:`twist <twist>`                                                                                        Specify the blade twist at blade section.

:ref:`airfoil_data_file <airfoil_data_file>`                                                  Specify the airfoil data file (cl/cd) at blade section.

============================================   ======================================================================================================

.. rubric:: Included in:

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Parent                                                                                   Summary

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:ref:`geometry_2 <geometry_2>`       Main menu to define a blade section in the current rotor:  

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