Airfoil with C-Spar

Airfoil example with a C-spar internal structure.

Notes

This case builds an airfoil cross-section with a C-spar layout. It is a compact example for validating spar topology and the interaction between the airfoil outline and internal structural members.

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Input

• cs_main.xml

• sc1095.dat

• material_database_us_ft.xml

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Run the example

prevabs -i cs_main.xml --hm

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Output

Figure 35 Cross section viewed in gmsh.

• cs_main.png