Set up your own cloud-native simulation in minutes.Start Simulating Now
Wing with Spiroidal Winglet
349
0
Statistics
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.
