If you are asking how an aircraft produces lift, it is quite simple. The shape of the wing causes there to be higher air pressure below the wing than above; causing the wing to rise up, to the area of least resistance.
The weight of an aircraft counteracts the lift produced by an aircraft. The heavier an aircraft weighs the greater the lift needed to get off the ground.
The only 'wingless aircraft' are helicopters. These produce lift lift from the rotor blades, which are in fact, long narrow wings.
The lift force is the force acting against the aircraft's weight. For straight and level flight, lift acts in the upward vertical direction and the weight of the aircraft acts in the downward vertical direction. For level flight, lift = weight.
A rotory aircraft is essentially a helicopter or a type of aircraft that relies on the movement of its wing to produce lift.
Lift balances weight. Thrust balances drag.
An aircraft propeller is what gives the aircraft power to move it forward (or backward, depending on it's pitch). This enables the aircraft to acquire lift and gain altitude. Propellers are found on some fixed-wing aircraft and autogyros. On helicopters, the blades that lift it and stabilize it are called rotors.
Lift.
Maximizing the lift-to-drag ratio is desirable because it allows an aircraft to generate more lift for a given amount of drag, resulting in improved fuel efficiency and range. A higher lift-to-drag ratio also means the aircraft can fly at higher altitudes and speeds, which can be beneficial for performance and overall aircraft capabilities.
The engines provide forward thrust, allowing the wings to generate lift. It is the lift that allows the aircraft to take off.
Flaps are used on aircraft to increase the wing area of the plane and therefore increase lift and reduce speed.
Gravity is the force that pulls an aircraft towards the ground, acting against the force of lift generated by the wings in level flight. Gravity pulls the aircraft downward, while lift generated by the wings counteracts this force to keep the aircraft aloft.
The total net force on an aircraft in flight is usually studied in terms of four perpendicular componentsreferred to as lift, weight, thrust, and drag.