Thiendrah said:So we got our force FnXsinQ=m.a=m.(vXv)/r, also the other component is "mg", so
when you divide those two, you will get mvv/gr.
Circular motion in an airplane refers to the movement of an airplane along a curved path or trajectory, rather than a straight line. This type of motion is typically seen when an airplane is turning, banking, or following a circular flight pattern.
In order to maintain circular motion, an airplane needs to have a centripetal force acting on it. This force is directed towards the center of the circular path and is provided by the wing design and the pilot's control inputs. The airplane's velocity and angle of bank also play a role in maintaining circular motion.
The radius of an airplane's circular motion is affected by the airplane's speed, angle of bank, and the strength of the centripetal force. A higher speed or steeper angle of bank will result in a smaller radius, while a lower speed or shallower angle of bank will result in a larger radius.
In circular motion, the centripetal force acts perpendicular to the velocity of the airplane, while the weight acts vertically downwards. This means that the centripetal force does not contribute to the lift of the airplane, but rather helps to balance out the weight. The lift of the airplane is still provided by the wings, which need to generate enough lift to counteract the weight and provide the necessary centripetal force for circular motion.
Yes, an airplane can experience circular motion in the vertical direction, such as when performing a vertical loop. In this case, the lift force from the wings must be greater than the weight of the airplane in order to provide the necessary centripetal force for circular motion. However, this type of circular motion is typically not sustained for extended periods of time due to the high energy requirements.