Correct answer is (a) True
Easy explanation: The minimum drag speed determines the best operating speeds of aircraft with thrust producing engines. The correct equation for minimum speed drag is Vemd=\(\sqrt[4]{\frac{ZW^2}{Y}}\) where Y is a constant, V is velocity, W is weight, Y is a constant and Vemd is minimum speed drag. Induced drag is the function of lift and caused when an aircraft is moving in the air.