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Computed Flows at Angle = 0
Computed Conditions – Geometry
Calculated Force Coefficients
Velocity Distribution on Canard
Velocity Distribution on Canard
Velocity Distribution on Lower Wing
Velocity Distribution on Lower Wing
Velocity Distribution on Upper Wing
Velocity Distribution on Upper Wing
Pressure Distribution on Canard
Pressure Distribution on Canard
Pressure Distribution on Lower Wing
Pressure Distribution on Lower Wing
Distribution on Upper Wing
Distribution on Upper Wing
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