... [35.5p5f8 x 16 480 + 55 .8 x lo5 - 55 .8 x I05pj4f5 55 .8 x 105 i.e. 55 .8 465 5f4 - 55 .8 x lo5 = (35.6 - 55 .8) 105 ( 0.1 488 ) 5 .84 - 55 .8 x 1oSp = or 55 .8~ - 5 .84 ~~1~ ... Aerodynamics for Engineering Students Pi 0.9 0 .8 0.7 - 0.6 0.5 - 0.4 - 0.3 - - - U - 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0 .8 1.0 0.9 0 .8 0.7 - 0.6 0.5 - 0.4 - 0.3 - - - ... 8, 30 1-3 08. A.R. Wazzan, C. Gazley and A.M.O. Smith (1 981 ) 'H-R, method for predicting transition', AZAA J., 19, 81 0412. 420 Aerodynamics for Engineering Students Aerodynamics...