Originally Posted by
Bernardo
To give some numbers:
Let's assume the airplane weighs 50,000 N (VLJ type aircraft).
Let's assume the airplane has 5,000 N of thrust.
Let's assume the airplane has a wing surface area of 20 sq.m.
Let's assume the rolling wheel-friction coefficient is 0.01
Let's assume the wing coefficient of lift is 1.5.
Lift = (1/2) * (airdensity) * (speed^2) * (coefficient of lift)
VTo = 1.2 * Sqrt( (Weight / Surface) * (2 / (density*(coefficient of lift))) ) = 60 m/s = 220km/h = 140mph
Thus, the aircraft has to reach 140mph AIR SPEED to achieve take off.
The roll friction drag is going to be negligible compared to the thrust of the engines, and thus it will not make any difference whether the airplane is on a rolling threadmill or on a static runway.
The airplane will have to accelerate to 140mph AIRSPEED, which will take the same time on either type of runway. Airspeed is entirely independent of ground speed.
Consider the following scenario: The treadmill starts rolling with the jet engines off. The airplane starts rolling backwards. Now, the pilot engages the jet engines, but with barely enough thrust to keep the airplane stationary. This will be ~1-2% available thrust.
In this case, the airplane isn't moving w/ respect to the air, but it is rolling on the threadmill. Even if the threadmill accelerates, the friction drag is going to be approximately the same, and no thrust increase is necessary.
Now, the pilot pushes the throttle to 100% available thrust. The jet engines easily overcome the friction drag from the treadmill, and the jet accelerates with respect to the rolling runway, and eventually takes off.