Wind tunnel tests have been made to investigate the influence of the jets from several different nozzles on the pressure distribution on adjacent wing panels with supercritical profiles. In Part I, an existing unswept wing ...

A method of calculating the velocity distribution in incompressible flow on annular aerofoils of moderate thickness/chord ratio and camber, and reasonably large radius/chord ratio (the order of 1 or greater), is developed, ...

A simple method of calculating the pressure distribution in incompressible flow on two-dimensional aerofoils of arbitrary section at moderate distances from the ground is developed. Comparisons with an 'exact' potential-flow ...