Surface pressure distribution over a delta wing            

The pressure on the windward side is due to
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The delta wing stalls at higher angles of attack because the vortex breakdown location is in the wake.
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At small angles of attack, the suction pressure develops on the upper surface of the delta wing.
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The aspect ratio of a delta wing with a sweep angle of 60 degrees and a root chord of 20 cm is
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The pressure coefficient is given by

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