el cid again -> RE: Aircraft Maneuverability (Japan added/Updated) (3/4/2006 5:48:16 PM)
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quote:
However, for high performance twin engined fighters like P-38, F7F and the like what would the results be if you did not devide by 2? They would be about twice as high (neglecting the impact of fractions which might subtract one from a doubling in some cases). Note, however, this is not just true of "high performance twin engined fighters" - it would be true for ALL twin engined (and presumably four engined) planes. The RELATIVE advantage of a twin engine fighter vs a twin engine bomber would be the same. The relative advantage of a twin engine fighter vs a four engine bomber would only be HALF. This would distort the reality insofar as twin engine night fighters really were effective against four engine bombers, even if they were only marginally better than twin engine bombers (which mostly they derived from). A high performance twin engine plane is modeled here more or less correctly: it is BETTER than a twin engine bomber - because it has a better power ratio and better ROC. Note I have increased the proportion of the non-speed component in the maneuverability rating, and this in particular benefitted high performance twin engine fighters. Heavier planes stayed anchored at the same values, but these gained points. And similarly a 4 engine plane would be four times as high. This results in preposterous values. Further, if you take the cases of planes which were used in more than one role - in particular bombers that were able to operate as night fighters - or night fighters that were intruder bombers - you will find that the maneuverability of these planes is in the same class as other twin engine aircraft, not single engine aircraft. Yet in the stock system, such aircraft were rated entirely differently - they divided a B-25 by 2 but not a twin engine fighter or night fighter. This was deliberately to address the concerns of those who wanted better performance for fighters I am sure. But it is the wrong way to proceed: Joe (who knew he was going to be able to do code) said "Get the database right first and we will get the code right next and then everything will be right." An aircraft is represented by a set of values - not one value. You may not correctly think of a plane if you are not considering ALL its fields at the same time. P-38s are going to do well because (a) their maneuverability is good relative to other twin engine aircraft and very good vs four engine aircraft; (b) they have great firepower - when they do get to shoot head on it is not nice to be in the way; (c) they have higher durability than any single engine plane - if they get hit they are much more likely to stay around for another round - or at least to go home and survive. PV-1 Ventura night fighters are much more marginal because their maneuverability is less - in spite of also having fair firepower and durability ratings. That said, it would be better to have a different algorithm for maneuverability. Since we cannot really test all these 240 planes to measure values, we probably cannot use the ideal data set: sustained rate of turn data is not recorded for most of them. But we can easily use weight, power and wing area to calculate wing loading and power loading - and we could combine these with initial ROC data in some way. HOW to do that well could take a long time to understand - but in principle this is better than the simplistic algorithms I have discussed here - and it is my plan to consider this for the next round of RHS. Right now I want a system that is based on real data and says, approximately, that maneuverability is better for small planes than big ones, etc. This to permit testing of the entire revised set of weapons, durability etc.
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