1. The problem statement, all variables and given/known data A pilot with mass m fles an airplane at a speed of v in a turn of radius r. Prove that angle of the wings of the airplane to the horizontal is tanQ=(VxV)/gr 2. Relevant equations 3. The attempt at a solution This was asked on my first exam last week. Since it's tangent. All we need to get is the force, result will equal to (FxcosQ)/(FxSinQ)=(VxV)/gr? I'm not getting anywhere with this? Can someone help me?