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.
Operating the ailerons will cause the aircraft to roll.
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.
They roll due to the thrust of the Aircraft during taxi and take off. They roll on landing due to weight of the Aircraft transferred to the tires and it's speed at touch down. There is no drive shaft to roll the wheels only the energy in the airframe and powerplants.
A pilot uses a yoke or joystick (depends what brand of aircraft they fly. joystick only really seen on military or airbus series) to control the ailerons which cause the aircraft to roll if need be