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55 degree leading edge sweep angle
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2 Geometries
1 Mesh
1 Simulation setup
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2 Geometries 1 Mesh 1 Simulation setup 0 ResultsAbout this project
An aerodynamic analysis of the vortex breakdown occurring over a delta wing with leading edge sweep angle of 55 degrees.
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Project History
tkenchington created this project
over 2 years ago
