probably a stall, but they are not that dangerous, if you are trained to get out of them
The speed of the rotor directly affects the amount of lift generated by a rotorcraft. As the rotor spins faster, it creates more lift by generating greater airflow over the rotor blades, allowing the aircraft to climb or maintain altitude. Conversely, decreasing the rotor speed reduces lift, potentially causing the aircraft to descend.
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.
Yes, lift is an unbalanced force. It acts in opposition to the weight of an aircraft, allowing it to rise or remain in the air. When the lift generated by the wings exceeds the gravitational force acting on the aircraft, the result is an upward acceleration. Conversely, if lift is less than weight, the aircraft will descend.
Lift balances weight. Thrust balances drag.
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.
Angle of attack may be negative or positive - it's simply the angle between the wing chord line and the oncoming airflow. If it's positive then the aircraft will benefit from the lift that is provided, if it's negative then there is no lift (but there's still drag). This is a potentially dangerous situation, unless you wish your aircraft to descend.
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 speed of the rotor directly affects the amount of lift generated by a rotorcraft. As the rotor spins faster, it creates more lift by generating greater airflow over the rotor blades, allowing the aircraft to climb or maintain altitude. Conversely, decreasing the rotor speed reduces lift, potentially causing the aircraft to descend.
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.
If an airplane exceeds it's maximum angle of attack, or drops below a certain velocity aerodynamic STALL is what occurs. It is characterized by separation of the flow over the top surface of the wing. This phenomenon reduces lift which, if designed right, will cause the aircraft to nose dive. That being said, stall for most airplanes is really only dangerous during take off and landing since there's not much vertical space to recover from the sudden loss of lift.
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.