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Computed Flows at Angle = 5

Computed Conditions – Geometry

Image of calculated force coefficients

Velocity Distribution on Canard

Image of velocity distribution on canard

Velocity Distribution on Lower Wing

Image of velocity distribution from lower wing

Velocity Distribution on Upper Wing

Image of velocity distribution on upper wing

Pressure Distribution on Canard

Image of pressure distribution on canard

Pressure Distribution on Lower Wing

Image of pressure distribution on lower wing

Distribution on Upper Wing

Image of distribution on upper wing

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