Airfoil with D-Spar

Airfoil example with a D-spar internal structure.

Notes

This case builds an airfoil cross-section with a D-spar layout. It is a useful comparison point against the C-spar example when checking baseline partitioning and mesh quality.

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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 36 Cross section viewed in gmsh.

• cs_main.png