1. Plot the curve for the section lift coefficient ?? ?? as a function of the angle of attack ?? for

1. Plot the curve for the section lift coefficient ____ as a function of the angle of attack __ for a thin foil section with parabolic mean line and a camber–chord length ratio of __0___ = 1.5%. 2. Compute and plot the dimensionless pressure distribution over the chord length for upper and lower side of a flat plate at an angle of attack __ = 3 degree.