Distiller -> RE: Aircraft 'Manuever' (8/6/2006 1:22:36 PM)
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quote:
ORIGINAL: el cid again I think you have a point. I do not understand it. Please amplify and clarify. What are "transient values?" And why does it matter if we cannot determine them? aircraft specs usually contain static values, ie. sustained climb, sustained turn and sustained roll rate. roll or turn rate do not build up in an instant, at the very least, inertia has to be overcome and some aircraft tend to dislike certain combinations like rolling out of high G turns, in which case roll rate may drop severely, even if it's sky high in the standard test, which is flown level, without G's. so, even if the Corsair rolls within a few seconds (360 deg roll), it's rarely done, ~90deg are used more often to initiate a hard turn, but the real question is how long does it take our simulated aircraft to roll a mere 10 or 15 degrees - at high g loads, preferably. roll rate is not a constant, it varies with time (increases with time until it reaches the published value), the question is how quickly this transition occurs. while a slowly rolling / turning plane will not magically outmaneuver one with high turn/roll rate, if both have similar book specs, rate of change may very well be the deceisive factor. of course, there's more to it, especially considering we're talking about propeller driven planes, which exhibit predictable asymmetrical rolling characteristics - unless you're using counter-rotating props, like the P-38J or later models, which therefore deserves a higher mvr value and that's before you take its dive brakes into account - effectively reducing the pilot's options and therefore our single, abstracted maneuver value. the Corsair may be unable to compete with a Zero in sustained turn, but it won't matter if it can keep up for a quarter turn with combat flaps, in the case of a miss, high excess speed and high speed handling allow a quick escape, while the Zero pilot is busy dodging and if he hits, the game's over.
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