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Wing with Spiroidal Winglet
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2 Geometries
1 Mesh
1 Simulation setup
1 Result
2 Geometries 1 Mesh 1 Simulation setup 1 ResultAbout this project
The purpose of this project is to study the influence of different types of winglets placed at the end of a commercial aircraft wing during takeoff. The flow will be considered incompressible and turbulent (kw-sst). The aerodynamic characteristics of the flow (lift, drag, eddies, etc.) will be determined.
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lmessaoudi created this project