LIFT 1.50 30 30 1.25- .25 1.00. COFFELCLENT .75 .50 .25 -10 O DRAC .20 20 COEFFICIENT .15 Clark Y Lift and drag .10 59 .05 25 25 30 30 ANGLE OF ATTACK $1 If this plane is capable of level flight (at an angle of attack of 0) at 300m s Approximately what angle of attack would be needed to produce the same lift at 150 m s? -5 5 10 15 20 20 P The lift coefficient is 1