Wind tunnel tests at Mach numbers between 0.6 and 1.4 of a 60° swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1.2.
Lawlor, E. F.,author.
Great Britain.Her Majesty's Stationery Office.
Aeronautical Research Council (Great Britain),issuing body.
May, 1961.