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8AR, 0.6TR, 0.35aC
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Statistics
1 Geometry
1 Mesh
1 Simulation setup
0 Results
1 Geometry 1 Mesh 1 Simulation setup 0 ResultsAbout this project
Confirmation of XFLR5 results for a wing with 8AR, 0.6 taper ratio, and 0.35 average chord. Comparison of drag and lift results at 0 AOA with 20 m/s free stream velocity.
