A two dimensional double wedge airfoil of semi wedge angle 8.0° is placed at zero angle of attack…

A two dimensional double wedge airfoil of semi wedge angle 8.0° is placed at zero angle of attack in a Mach 3.0 supersonic wind tunnel. That should be the minimum height of the wind tunnel test section in terms of the chord so that the reflections of the oblique shock formed at the leading edge of the model does not disturb the model.

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