Tests of a Griffith aerofoil in the 13 ft. x 9 ft. wind tunnel.
Great Britain.Ministry of Supply,issuing body.
Great Britain.His Majesty's Stationery Office.
March, 1944.
Part I. Wind tunnel technique and interim note -- part II. Effect of concavity on drag -- part III. Effects of wide slots and of premature transition to turbulence -- part IV. Lift, drag, pitching moments and velocity distributions.