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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. 5TH ANNIVERSARY OFFICE OF TRAINING

   vanished, the Of- fice of Training seized on the opportunity to advance its Approved For Release 2002/11/01: ...

3. 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 ...