Inlet guide vanes add swirl to change the incidence angle at the inlet of the impeller. With a constant speed compressor, the velocity triangle at the inlet is a function of the tip speed at the eye and the gas velocity. The angle of the blade at the inlet (Beta) is designed to minimize incidence at the design flow, at low flows the incidence angle is not optimum due to the low inlet velocity (and the blade geometry is fixed). IGV's induce swirl to reduce incidence and increase the range of the compressor. As incidence is reduced, so is head.