KillerCharlie
Diamond Member
- Aug 21, 2005
- 3,691
- 68
- 91
First of all, I will begin this by saying I'm an aerospace engineer. More specifically, I'm an aerodynamicist for Boeing. I analyze and help design the aerodynamic configuration for commercial planes. Take my word for what it is, but it's obvious that lots of people here are spewing crap out of their butt and don't have a background in science and engineering. I work in designing the shape of the aircraft and am not a performance engineer. I know some people who work in performance, but I don't personally know anyone who works with takeoff performance. There are a couple points I must make.
First of all, the question is poorly worded. Whoever wrote it is an idiot and needs to learn how to write questions that a well-posed. There are 2 interpretations I have seen:
1) The treadmill keeps the plane from moving in the reference frame of an observing sitting on the ground (not standing on the treadmill)
2) The treadmill just goes the opposite speed of the airplane
For condition 1, the answer is obvious - no lift because of no airflow over the wing. For condition 2, if the airplane goes forward, then you can takeoff. The problem here is determining if the aircraft can go forward.
Here is how aircraft are typically modeled for takeoff:
Forces acting on aircraft:
Lift upwards (proportional to V^2)
Weight downward, thrust forward, drag backwards, and resistance from the wheels pulling you backward as well.
The resistance force from the wheels, as a first approximation, is proportional only to the normal force on the aircraft (weight-lift) and nothing more. Therefore, the treadmill does not do anything.
Of course, a higher-fidelity model for wheel resistance will include things like tire rotational speed, tire air pressure, and so on. However, the resulting changes are small. I'd love to ask a performance engineer how they calculate these things, but I have the feeling they just do it with a flight test and don't worry about the physics of it.
Oh, and AlienCraft, pitot tubes do not measure groundspeed. It will not read 30mph - your airspeed indicator will read 130 mph. Your relative airspeed it what matters, not ground speed. Some advanced aircraft can get their ground speed using things such as GPS. Also, determining airspeed from a pitot tube does NOT require any differential equations.
First of all, the question is poorly worded. Whoever wrote it is an idiot and needs to learn how to write questions that a well-posed. There are 2 interpretations I have seen:
1) The treadmill keeps the plane from moving in the reference frame of an observing sitting on the ground (not standing on the treadmill)
2) The treadmill just goes the opposite speed of the airplane
For condition 1, the answer is obvious - no lift because of no airflow over the wing. For condition 2, if the airplane goes forward, then you can takeoff. The problem here is determining if the aircraft can go forward.
Here is how aircraft are typically modeled for takeoff:
Forces acting on aircraft:
Lift upwards (proportional to V^2)
Weight downward, thrust forward, drag backwards, and resistance from the wheels pulling you backward as well.
The resistance force from the wheels, as a first approximation, is proportional only to the normal force on the aircraft (weight-lift) and nothing more. Therefore, the treadmill does not do anything.
Of course, a higher-fidelity model for wheel resistance will include things like tire rotational speed, tire air pressure, and so on. However, the resulting changes are small. I'd love to ask a performance engineer how they calculate these things, but I have the feeling they just do it with a flight test and don't worry about the physics of it.
Oh, and AlienCraft, pitot tubes do not measure groundspeed. It will not read 30mph - your airspeed indicator will read 130 mph. Your relative airspeed it what matters, not ground speed. Some advanced aircraft can get their ground speed using things such as GPS. Also, determining airspeed from a pitot tube does NOT require any differential equations.