The coordinated pair of ailerons does.
A roll in a vehicle or aircraft is caused by an imbalance in lift or forces acting on one side of the vehicle or aircraft compared to the other. This imbalance can be due to factors such as uneven weight distribution, aerodynamic forces, or control inputs.
A smooth and flat surface with minimal friction, such as a polished marble floor, will allow a ball to roll the fastest. The lack of friction will reduce resistance and enable the ball to maintain its speed for longer distances.
A basketball will roll faster on a smooth surface due to less friction compared to a rough surface. The rough surface creates more resistance, slowing down the ball's movement.
Marbles roll due to a combination of gravitational force pulling them downward and frictional forces between the marble and the surface it is rolling on. If the surface is smooth, gravity will dominate and the marble will roll faster. If the surface is rough, friction may slow down the marble's rolling.
The ball with the least amount of friction will roll the farthest. This typically means a ball with a smooth and spherical surface. The surface on which the ball is rolling will also affect its distance.
At the outer ends of the wings are 'ailerons'. These are like flaps, but when one goes up, the other goes down, thus the aircraft rolls.
Aircraft are able to turn left to right, vice versa or around by controlling the spin of the wheels. Preventing the right wheels to roll will turn the aircraft to right and controlling the left wheels will make a left turn.
The right aileron is a control surface on an aircraft's wing that helps manage roll. When the right aileron is deflected upward, it decreases lift on the right wing, causing the aircraft to roll to the left. Conversely, when it is deflected downward, it increases lift on the right wing, causing the aircraft to roll to the right. This allows pilots to control the aircraft's orientation during flight.
Operating the ailerons will cause the aircraft to roll.
Aileron power refers to the effectiveness and responsiveness of an aircraft's ailerons in controlling roll movements. It is a measure of how quickly and accurately an aircraft can change its orientation about the longitudinal axis in response to pilot inputs. Factors influencing aileron power include the design of the ailerons, the aircraft's speed, and its overall aerodynamic characteristics. High aileron power allows for more agile maneuvering, especially in aerobatic or high-performance aircraft.
Elevators control the pitch (up and down) of the aircraft. Ailerons control the roll of the aircraft. And rudders control the yaw of the aircraft.
Kempton H. Roll has written: 'Controlling corrosive air pollutants'
That is when the aircraft rotates around it's axis.
A roll in a vehicle or aircraft is caused by an imbalance in lift or forces acting on one side of the vehicle or aircraft compared to the other. This imbalance can be due to factors such as uneven weight distribution, aerodynamic forces, or control inputs.
Dutch roll is the tendency of an aircraft to roll and yaw about its longitudinal and vertical axis due to inherent instability in the design of the aircraft. Generally it is the result of a small vertical stabilizer design.
Pitch is a rotating movement of the body of the aircraft about the axis of the wings. Pitch is represented by rotating to tilt the aircraft up or down. Yaw is a rotation left and right, similar to turning your head to the left and right. Roll is a rotation of the aircraft about the front to rear axis. An aircraft would roll if the pilot wanted to turn it to fly upside down.
Roll, pitch, and yaw - flight dynamics. See the below link for more info.