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1 Geometry
1 Mesh
1 Simulation setup
1 ResultIllustrative structural analysis of a 2.5 m aluminium wing. Assumed vertical airflow 25 m/s, equivalent air load 490 Pa. Not an airworthiness assessment.
rene01bbw created this project
about 1 month ago
1 Geometry 1 Mesh 1 Simulation setup 1 ResultIllustrative structural analysis of a 2.5 m aluminium wing. Assumed vertical airflow 25 m/s, equivalent air load 490 Pa. Not an airworthiness assessment.
by slilbaekslilbaek
