In order for an airplane to achieve lift off, the force of lift must be greater than that of its weight and the drag of the air (neglected). In this Demonstration, you can change the type of airplane, wing area, and city the airplane is in to see the necessary velocity the airplane must reach in order to lift off. The change of airplane affects the weight of the airplane and coefficient of lift, and the change of city affects the air density. These three factors and the wing area are used in computing the velocity an airplane needs in order to achieve lift off. See how the variables correlate with lift off velocity.

Lift can be calculated using the equation , where is the force of the lift, is the wing area (), is the air density, is the coefficient of lift, and is velocity.

The force of lift is equivalent to the weight of the aircraft when at equilibrium in a fluid. Therefore, as long as the lift is greater than the weight of the aircraft, the aircraft ascends. The drop-down menu of the different airplanes determines the weight and the coefficient of lift.

The air density depends on the chosen city. Each city corresponds to an air density that was calculated using weather data on May 22, 2016, 12:00 EST.

Choose the inputs to see the velocity.

This Demonstration does not take into account the effects of drag.