D. G. Hurley

• A note on the cause of the nose stall of thin wings
• A series of aerofoils designed to develop exceptionally large lift coefficients when boundary layer control by blowing is employed
• Experiments on the effects of air jets and surface roughness on the boundary layer near the nose of an N.A.C.A. 64A006 aerofoil
• Experiments on the effects of air jets and surface roughness on the stalling characteristics of a 5 ft. chord NACA 64A006 aerofoil
• Note on the forces that act near the centre and the tips of swept wings
• On rotating curved discs
• The development of flow separations on the Avro 707A aircraft: a comparison of wind tunnel and flight based on the measurement of surface pressures
• The downstream effect of a local thickening of the laminar boundary layer
• The effect of surface roughness on the stalling characteristics of a thin aerofoil