W.T. Lord; G.K. Hunt; R.J. Pallant; J. Turner
(1954)
This report presents distributions of Mach number in the empty working section of the R.A.E. No. 18 (9" x 9") Supersonic Wind Tunnel at nominal Mach numbers of 1.4, 1.5, 1.6, 1.8 and 1.9, for condensation-free flow at ...