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Wing with Spiroidal Winglet

Wing with Spiroidal  Winglet image
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lmessaoudi
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geometries 2 Geometries
meshes 1 Mesh
simulations 1 Simulation setup
runs 1 Result

About 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.