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1 Geometry
1 Mesh
1 Simulation setup
0 ResultsPressure Distribution: Clear low-pressure region over upper wing surface indicating lift generation Velocity Distribution: Streamlines show smooth acceleration over airfoil and controlled wake Forces Obtained: Lift ≈ 32 N Drag ≈ 4.5 N 𝐿 𝐷 D L Ratio ≈ 7.1
by slilbaekslilbaek
Kavitha24 created this project
about 1 year ago
1 Geometry 1 Mesh 1 Simulation setup 0 ResultsPressure Distribution: Clear low-pressure region over upper wing surface indicating lift generation Velocity Distribution: Streamlines show smooth acceleration over airfoil and controlled wake Forces Obtained: Lift ≈ 32 N Drag ≈ 4.5 N 𝐿 𝐷 D L Ratio ≈ 7.1
