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  1. TURBULENT BOUNDARY LAYERS ON DELTA WINGS AT ZERO LIFT

    would have reduced to 1+ 1 1 g n Cep = n+1 C R n- C1 + 0- 1281.1 c- c (;, (2) n 00 s assuming 6 to vanish ... but this is generally ignored.) Now from Table 1 2+ H-M2 = 3.5-0.555M2 and this vanishes when Iii = 2.51, ...

  2. MEASUREMENTS, AT MACH NUMBERS UP TO 2.8, OF THE LONGITUDINAL CHARACTERISTICS OF ONE PLANE AND THREE CAMBERED SLENDER OGEE WINGS

    at the leading edge and at the centre is chosen such that the load vanishes at the leading edge. The ordinates ...