Climb - Climb Operation

Climb Operation

A climb is carried out by increasing the lift of airfoils (wings) supporting the aircraft until their lifting force exceeds the weight of the aircraft. Once this occurs, the aircraft will climb to a higher altitude until the lifting force and weight are again in balance. The increase in lift may be accomplished by increasing the angle of attack of the wings, by increasing the thrust of the engines to increase speed (thereby increasing lift), by increasing the surface area or shape of the wing to produce greater lift, or by some combination of these techniques. In most cases, engine thrust and angle of attack are simultaneously increased to produce a climb.

Because lift diminishes with decreasing air density, a climb, once initiated, will end by itself when the diminishing lift with increasing altitude drops to a point that equals the weight of the aircraft. At that point, the aircraft will return to level flight at a constant altitude.

However, during a constant rate climb at a reasonably steady angle the lift force is generally less than the weight with the engine operating. This is due to the upward fraction of the thrust vector. This in turn causes the load factor to be slightly less than 1. It is only during the radial (constant increase in pitch) or vertical acceleration that the lift vector is larger than the weight vector.