wikipedia said:The term rotation is used because the aircraft pivots around the axis of its main landing gear while still on the ground, usually due to manipulation of the flight controls to make this change in aircraft attitude.
Rotation (Vr) by no means represents the moment the aircraft leaves the ground. That would be 'lift off' speed.
It strictly refers to the speed that the nose wheel leaves the runway and the plane is pitched to the takeoff attitude.
Of course, I'm not flying Jets either. Might be something different there...
Rotation (Vr) by no means represents the moment the aircraft leaves the ground. That would be 'lift off' speed.
It strictly refers to the speed that the nose wheel leaves the runway and the plane is pitched to the takeoff attitude.
Of course, I'm not flying Jets either. Might be something different there...
Despite my poor choice of words, I know that rotation happens when the nose leaves the ground. My question was why it was called rotation. The answer apparently being "because the aircraft pivots around the axis of its main landing gear".
This ensures that the airplane will fly and keeps me from dragging the tail if we have a bunch of fatties in the back whose weight wasnt accounted for....
As far as the physics of it.... during the first part of rotation you are pitching around the main wheel trucks.... they are situated aft of the true lateral axis. Once the weight is relieved off of the trucks, then you are pitching directly around the lateral axis of the aircraft.
The action taken at "rotate" speed is simply to begin to bring the aircraft's nose up during the takeoff roll. Derotate is what you do during the flare when you bring the nose back down to the ground.
The speed that "rotate" is called during a large aircraft's takeoff roll is the calculated speed to get the aircraft into the air and stabilize at the appropriate pitch attitude to maintain V2+10 to 15 with a 2 degree per second rate of pitch up.
This is theoretical of course....in real life, on both the 757 and 767 I bring the nose to 7.5-9 degrees nose up and stop rotation until I break ground. This ensures that the airplane will fly and keeps me from dragging the tail if we have a bunch of fatties in the back whose weight wasnt accounted for... Once I break ground, then I continue pitch up to normal attitude (15-20 degrees nose up typically).
As far as the physics of it.... during the first part of rotation you are pitching around the main wheel trucks.... they are situated aft of the true lateral axis. Once the weight is relieved off of the trucks, then you are pitching directly around the lateral axis of the aircraft.
This is theoretical of course....in real life, on both the 757 and 767 I bring the nose to 7.5-9 degrees nose up and stop rotation until I break ground. This ensures that the airplane will fly and keeps me from dragging the tail if we have a bunch of fatties in the back whose weight wasnt accounted for... Once I break ground, then I continue pitch up to normal attitude (15-20 degrees nose up typically).
Rudder? That's for when you lose an engine right?It still even follows the laws of physics like coordinated turns and ground effect. Though those two get forgotten about a LOT around here.