Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing /
Black, J.,author.
Great Britain.His Majesty's Stationery Office.
Aeronautical Research Council (Great Britain)
"Dec. 22, 1952."
Pt. I. Three-dimensional tests on the wing -- pt. II. Two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section.