Originally posted by twhitehead
But that is assuming it is accelerating horizontally. We were told quite clearly that it accelerating at 12 degrees.
Acceleration=rate of change of velocity.
velocity=rate of change of position.
if position=0 and velocity=0 and acceleration exists then movement is instantaneous in the direction of the acceleration ie 12 degrees.
Therefore the plane takes off immediately.
You have a bit of a dilemma, the problem is stated wrong. You cannot have a plane take off immediately with less than a quarter G of acceleration.
You seem to forget the earth imparts 1 full G of force downwards. So with 1/4 G going upwards, it doesn't take a rocket scientist to see the plane can only act like a car and move forward. The problem says the plane comes in at 175,000 pounds or Kg, forget which, but either way, you get less than 50,000 pounds or Kg of thrust, which even if it was pointed straight up, would get you nowhere except to burn off a lot of fuel for nothing. At 12 degrees, you would have some vector of vertical force, maybe 1/8th of the total thrust going upwards but the majority of it would be spent moving the plane forward. Some people have said he probably means the wings are at a 12 degree angle, front end up, but that is not needed to generate vertical thrust, the differential pressures above and below the wing with sufficient air flow by the wing is what gives vertical lift. So you can maybe say the whole plane is on a tilted runway, tilted upwards at a 12 degree angle. If so, and my numbers are anywhere near correct, the 12 degree angle would consume maybe half the forward thrust giving a net acceleration of around 1 unit of accel instead of two and change which would at least double the length needed to get up to takeoff velocity. I am not doing any math, just trying to give an idea of the vectors involved.