Surface pressure distribution over a delta wing            

The suction peaks near the leading edge are due to the development of leading-edge vortices.
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With increasing angles of attack, the suction value in the trailing edge decreases due to the
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At the same angle of attack, the magnitude of suction peaks in the direction along the leading edge
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The delta wing stalls at
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Which component of the airflow induces the formation of the leading-edge vortex?
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