Hey
Well the question says u r in a steady flight so I assume lift equals weight. That means cl which is 0.42 is also the value for my weight and den since d angle of attack increased by 3° the cl becomes 0.72 but my weight remains 0.42 so load factor is 0.72/0.42=1.71 I hope u get it.
Last edited by avl998; 13th Feb 2015 at 05:59.
Reason: Correction it's not click it was cl **