Experimental Investigation of a 5% Thick Aerofoil with Sharp Leading and Trailing Edges, and Blowing Applied at the Mid-chord Point at Two Angles Relative to the Surface

Experimental Investigation of a 5% Thick Aerofoil with Sharp Leading and Trailing Edges, and Blowing Applied at the Mid-chord Point at Two Angles Relative to the Surface PDF Author: McGill University. Mechanical Engineering Research Laboratories
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Languages : en
Pages : 42

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