Will it take off?, page 2
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reply posted on 14-2-2006 @ 02:14 AM by Bhadhidar
Originally posted by Travellar
Originally posted by Bhadhidar


You were off to a good start, but the runway will not negate the speed of the aircraft, and it's speed is relative to the air.


The treadmill runway in the excercise was intended, as I read it, to negate any forward motion, speed (more precisely: ground-speed).

The ground, the plane on the ground, and the air above the ground all start with the same relative speed, 0 MPH.

The plane starts its engine. In normal operation, the plane then begins to gain speed, relative to the ground and the air above the ground, which are still at 0 MPH relative to each other. The plane's (forward) velocity through the air (still at a relative 0 MPH relative to the ground) moves a sufficient volume of air at a sufficient velocity over the wing's surface to provide adequate lift for take off.

If the surface upon which the plane is to taxi counter-acts the forward motion of the plane, which is what the theoretical "treadmill" in the excercise was designed to do, it effectively renders the plane motionless relative to the the actual ground (the Earth) and the air mass above it; no air will move over the wing, hence no lift. The plane will have no speed (0 MPH) relative to the air surrounding it.

If the plane cannot move forward, no matter how much thrust its engine is generating, because its wheels are essentially spinning in place, it cannot gernerate lift; it cannot fly.



reply posted on 14-2-2006 @ 05:27 AM by ch1466
Xerrog,

>>
Your right it will take off. A conveyor type system actually wont pull the plane back at all. It will not keep it from moving. A plane relies on air to push/pull itself forward not the wheels.
>>

WRONG.

And the proof is simple.

Assume it's a tractor-driven prop aircraft.

Say the 'P effect' of slipstream from a propellor acts against the airfoil (and fuselage) inboard of about the 1/2 span point sufficient to create lift enough for the plane to fly. If this wash is in effect the only fluidic behavior acting on the airframe as a function of 'powered lift', why waste the weight and _drag_ of the outboard span which is NOT under P Effect?

Particularly if the jet is not designed to have added maneuver much beyond 1G level flight.

Now assume it's a jet. If the wash (had damn well better be) aft of the wing /pushing/ it forward is only sufficient to keep it motionless, WHAT is generating the powered lift (propulsive fluid force directed over) ANY PART of the wings sufficient to provide lift?

Now assume it's a helicopter, if the helicopter needs only move forward at sufficient speeds that it's rotor acts as a fixed airfoil, why the wasted weight of a transmission and anti torque system to spin the main rotor for vertical takeoff?

Because the blades independent motion _faster than the forward motion of the aircraft_ is required to generate enhanced differential pressure and thus lift effect, that's why.

People like this assume that jet=thrust and thrust=lift where in, really, lift is based on relative motion THROUGH the air to create differential pressure GREATER than thrust.

Even if you are only 'pushing' with a quarter of the total mass-offset needed to push it (straight up) directly. The air holds you up. Thrust only parts it as a function of motion.

All motion in this hypothesis begins and ends with the frictional cancellation of energy through the rotational effect OF THE WHEELS. And it is their very lack of 'traction' (which is to say more torque from a motor than drag from the conveyor) _not friction_ that prevents them from ever overcoming the equal and opposed force sufficient to generate independent airfoil movement through the air.

So long as both conveyor belt and jet are cancelling each others applied forces (Newtonian Physics people) so that THE WING stays motionless, there is NO LIFT.

And no takeoff.

No matter how fast your wheels spin.


KPl.

[edit on 14-2-2006 by ch1466]


reply posted on 14-2-2006 @ 02:08 PM by G8tsoHellrOpn4me
Originally posted by ch1466
Xerrog,

>>
Your right it will take off. A conveyor type system actually wont pull the plane back at all. It will not keep it from moving. A plane relies on air to push/pull itself forward not the wheels.
>>

WRONG.

And the proof is simple.

Assume it's a tractor-driven prop aircraft.

Say the 'P effect' of slipstream from a propellor acts against the airfoil (and fuselage) inboard of about the 1/2 span point sufficient to create lift enough for the plane to fly. If this wash is in effect the only fluidic behavior acting on the airframe as a function of 'powered lift', why waste the weight and _drag_ of the outboard span which is NOT under P Effect?

Particularly if the jet is not designed to have added maneuver much beyond 1G level flight.

Now assume it's a jet. If the wash (had damn well better be) aft of the wing /pushing/ it forward is only sufficient to keep it motionless, WHAT is generating the powered lift (propulsive fluid force directed over) ANY PART of the wings sufficient to provide lift?

Now assume it's a helicopter, if the helicopter needs only move forward at sufficient speeds that it's rotor acts as a fixed airfoil, why the wasted weight of a transmission and anti torque system to spin the main rotor for vertical takeoff?

Because the blades independent motion _faster than the forward motion of the aircraft_ is required to generate enhanced differential pressure and thus lift effect, that's why.

People like this assume that jet=thrust and thrust=lift where in, really, lift is based on relative motion THROUGH the air to create differential pressure GREATER than thrust.

Even if you are only 'pushing' with a quarter of the total mass-offset needed to push it (straight up) directly. The air holds you up. Thrust only parts it as a function of motion.

All motion in this hypothesis begins and ends with the frictional cancellation of energy through the rotational effect OF THE WHEELS. And it is their very lack of 'traction' (which is to say more torque from a motor than drag from the conveyor) _not friction_ that prevents them from ever overcoming the equal and opposed force sufficient to generate independent airfoil movement through the air.

So long as both conveyor belt and jet are cancelling each others applied forces (Newtonian Physics people) so that THE WING stays motionless, there is NO LIFT.

And no takeoff.

No matter how fast your wheels spin.


KPl.

[edit on 14-2-2006 by ch1466]


As smart as your post attempts to make you sound, you are completely WRONG.

The wheels on a plane are there simply to support the aircraft while it is on the ground. They do not provide the force that moves the plane forward such as what a car would do. The force to move foward is provided soley by the propellor and/or jet engine against the air mass around the aircraft. Thus, the force of the engine against the air mass is not affected by wheels that are essentially free spinning and the aircraft would take off normally with just the speed of the wheels themselves being affected.

How else would planes take off on ice???
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