<p>This is what sky, who’s theory I am now supporting as opposed to my prop one, said when I asked him to post here for all of you from the Engineering Majors thread:</p>
<p>bmanbs2, </p>
<p>As much as I would like to, I don’t think I’d have the energy to enter another debate on this topic. </p>
<p>All the debate in the MIT thread is meaningless. The simple fact of the matter, this problem can be simply solved using the first thing they teach you in high school physics… using a free body diagram. An airplane will have 4 forces acting on it, thrust, drag, lift, and weight (due to gravity). Lift can be ignored for this problem. Let’s assume a stationary airmass along the “runway.” Obviously if you have a headwind, you can take off with a lower ground speed, but assuming it is stationary will make things easy (and is a perfectly fine assumption. Zero wind is a great condition for pilots). Aerodynamic drag will not become a significant force during the initial roll, so that can be ignored at first. Thrust of the engine will be assumed constant as a function of velocity. The only remaining forces we are looking at are the thrust of the engine and the frictional forces due to the landing gear. Without even looking at the mechanics of the frictional forces, I think it is pretty clear that the forces due to friction will be much much less than the forces due to the propulsion system. The net force in the longitudinal direction can mean only one thing in Newtonian physics: an acceleration. The airplane will continue to accelerate until the forces balance (no net force = no acceleration). Aerodynamic drag will certainly increase with velocity (squared), but the frictional forces at the tire and in the wheel bearings are dependent primarily upon forces acting normal to them (based on the weight), which will decrease as the airplane starts producing lift that opposes the weight. These frictional forces generally are independent of velocity. “Startup” forces that get bearings spinning are much higher than any friction that is caused by spinning the bearings faster (as what would happen when the treadmill speed increases). </p>
<p>Remember how we assumed a stationary airmass? As the airplane velocity increases (since it is accelerating down the runway), there is now a airflow over the wings which produces lift. Even if you don’t assume a stationary airmass, then you will get another velocity component between the wing and the airmass, but regardless, the airplane’s velocity is generally much higher than the airmass. </p>
<p>And with respect to your puller prop statement… It could help… but only in a certain configuration. The prop wash in a tractor (ie. puller) configuration can increase the lift a wing generates if the wing is in the slipstream of the propeller. Most pilots will know that the “power-on” approach can result in a lower airspeed as compared to the “power-off” approach. This is because a propeller does increase the airflow over the wings, and therefore does produce a bit more lift. However, for this problem, this fact is pretty much irrelevant.</p>
<p>Well… dang! It looks like in the time that it took me to write this, I could have posted the same message in the MIT forum. Regardless, if you want, you can link them to this post, or cut and paste it yourself.</p>
<p>I’ll also add my credentials as a pilot and aerospace engineer if it helps add any weight to my argument.</p>