1. The problem statement, all variables and given/known data Hi guys, i need some help solving the following question. An Airplane is flying in a Horizontal circle at speed of 620km/h. If the wings of the plane are tilted 35 degrees to the horizontal, what is the radius of the circle in which the plane is flying? Assume that the required force is provided entirely by an aerodynamic lift that is perpendicular to the wing surface. 2. Relevant equations 3. The attempt at a solution I know that if i had time i could find the radius by using R = vT/2pi But i dont have that so how would i go about solving this Problem? Also what can i do with that angle?