el cid again -> RE: How he got the new ratings (9/24/2006 6:10:47 AM)
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ORIGINAL: Herrbear quote:
ORIGINAL: el cid again quote:
ORIGINAL: Herrbear Something I just thought of concerning the dividing by the number of engines. Now that Wing Loading and Power Loading is taken into account do you penalize multi engine planes for speed and ROC. Wouldn't all planes, in theory, be consistent for those two factors. For example, shouldn't a 2-engine plane with 1000 hp engines with a ROC of 3000 and weight of 10,000 lbs work the same as a 1-engine plane with a 2000 hp engine also with a ROC of 3000 and a weight of 10,000 lbs. Why would the 2-engine plane be penalized in those factors? The multi engine penalty - it is not just for twin engine planes - but all of them - is meant to address the problem of conservation of angular momentum. It is meant to say that it is a severe restriction on maneuverability. It is a nice part of the function - whatever the number of engines - it goes there. There is, however, this caviet: multiple engines on one axis count as one engine. This can occur in 3 ways (and does NOT occur in WITP so far). 1) Two engines coupled to act as one. 2) Two engines with a common shaft - driving counter rotating screws on the same hub. 3) Two engines on a single axis - one driving a tractor and one a pusher. Anyway - the number of engines is in the deonominator because that is the right place for it to be. It divides what otherwise would be the maneuverability value - a composite function - by N. It is not meant to say any particular element of that function is so divided. Sid -- I understand why the penalty is used as it impacts wing loading and power loading. But does the "problem of conservation of angular momentum" have any impact on max speed or ROC. If it doesn't, why penalize those factors? The problem is you are being too analytical: I am NOT penalizing those factors. The number of engines is meant to affect the composite function - and it is not a comment on any particular other factor.
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