Hello,
I am no maths wizz, but I think you may have overlooked something:
1. The effect of inertia
2. The changing length of the beam
I am quoting in the following Donald R. Hill: Trebuchets
QUOTE(Liang Jieming @ Apr 27 2006, 09:53 PM) [snapback]4807214[/snapback]
The same traction catapult frame can be made to range further, throw heavier projectiles, projectile trajectory etc. simply by manipulating the pullers on the catapult ie. playing with the number of pullers as well as varying the way the ropes are pulled/held (within a reasonable range due to constraints like standing space and throwarm strength).
Actually, the more I play around with the equations and model larger sized catapults, I'm finding that the arbitrary 200m max range limit to a traction catapult is not so much the inability of the mechanism to reach larger ranges, but simply a logistical problem of fitting sufficient people under the catapult.
The counterweighted catapult allowed greater weights to be placed within the limited area and hence, broke the "max number of pullers" limit rather than the max range limit.
I been thinking and staring at the graphs for awhile now. The question that just begs to be asked is that whether a catapult design exists that would allow a traction crew to throw a decent sized projectile to the same ranges as the hinged counterweight catapults did. Surely they could since the only difference between the two was the counterweight pull force.
I do not think there are that much variables for a traction catapult.
1. I do not know what you mean with "varying the way the ropes are pulled/held". I would dispute that a large crew of dozens or even hundreds of men can make unisono subtle changes to influence the trajectory in any meaningful way. Hill for one finds that "with such large numbers, there must have been a high degree of training and discipline."
I would therefore rather say, for the motions of the pulling crew it is either all or nothing.
2. I dont see how the projectile trajectory can be influenced easier with a traction treb as it lacks a throwarm barrier and manipulating the release mechanism of a sling is as easy with an onager.
3. Playing with "the number of pullers" has also its limits. This is already obvious from the historical fact that in the initial report about Song catapults there were three different catapults: light, medium and heavy. Obviously, such a variety would not be necessary if the Song had felt they had an all-round catapult.
The physical reason seem to be inertia, which, as far as I can tell, is not part of your calculations: "In a counterweight trebuchet, for example, doubling the mass of the counterweight doubles its moment of inertia, while doubling its distance from the fulcrum quadruples its moment of inertia...exactly the same considerations can be made for the missile if it is resting on the end of the beam. In general, the same considerations also apply for the beam: increase in its mass increases its moment of inertia...an understanding of the basic concept of inertia and of the interdependence of all parts of a rotating body is essential to an understanding of the way trebuchets work."
Hill continues: "Huuri attempted to compare the power of the two machines (traction treb and CW treb) by imaginging the pulling crew loaded into the counterweight box, but rejected this line of reasoning because he felt that the weight of a man does not necessarily equal the pull he can exert. But this is the least of the reasons that make this argument absurd: the lightness of the beam due to the absence of a counterweight, the absence of inertia due to a counterweight, and the shortness of the pull are the essential factors that distinguish the traction trebuchet from the counterweight trebuchet."
And: "The three main components -counterweight, beam, and missile- are all parts of the same body. They combine to produce acceleration,
and they also combine to produce the total inertia that resists acceleration. Both the traction trebuchet and the counterweight trebuchet were compound pendulums but they operated under quite different dynamic conditions."
Thus, you cant equate both trebs like you did. There is no going on with larger and larger crews for the same machine. Instead, the length of the beam varies with the weight of the missile and the counterweight respectively the pulling crew. Hill gives for large machines a ratio of 3-1 or 2-1 between long and short arm and for small machines 5-1.