[rebel-builders] C of G change advice
Posted: Sun Feb 19, 2012 11:38 am
Hi Rick
Good to see that the Cheeze Grater is back on line ;-)
I don't have a cuffed airplane but, I'll take a crack at this just for fun.
1) The C of G should move forward my an almost unmeasurable amount - that is the (static) weight added by the cuffs will probably be added ahead of the previous C of G therefore moving it forward. I think you actually meant the centre of LIFT and it should move forward in proportion to the amount of wing area you added since the area added would be in
front of the previous C of L. I doubt that it would be a linear (with area) increase either since different parts of the wing contribute varied amounts of lift for a given area. Bottom line you may be able to lose some of that "balance enhancing mass".
2) Range of C of G. I think you're looking for an allowable C of G range increase and I think you're correct due to the added chord length. Since this is the first application of this design on this airframe you can now call yourself a test pilot! That'll be good for bragging at the pub!
3) You'll probably enjoy better low speed handling but as in 2), you'll have to do some testing to see how it turns out. Stalls may be different in nature from before.
Hope that rambling was useful!
Cheers,
Dave
Rick Harper wrote:
David A. Ricker
Fall River, Nova Scotia
Canada
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Good to see that the Cheeze Grater is back on line ;-)
I don't have a cuffed airplane but, I'll take a crack at this just for fun.
1) The C of G should move forward my an almost unmeasurable amount - that is the (static) weight added by the cuffs will probably be added ahead of the previous C of G therefore moving it forward. I think you actually meant the centre of LIFT and it should move forward in proportion to the amount of wing area you added since the area added would be in
front of the previous C of L. I doubt that it would be a linear (with area) increase either since different parts of the wing contribute varied amounts of lift for a given area. Bottom line you may be able to lose some of that "balance enhancing mass".
2) Range of C of G. I think you're looking for an allowable C of G range increase and I think you're correct due to the added chord length. Since this is the first application of this design on this airframe you can now call yourself a test pilot! That'll be good for bragging at the pub!
3) You'll probably enjoy better low speed handling but as in 2), you'll have to do some testing to see how it turns out. Stalls may be different in nature from before.
Hope that rambling was useful!
Cheers,
Dave
Rick Harper wrote:
--G'day from OZ Everyone !
We have just rebuilt our REBEL & received our new C of A & are just about to embark on a new flight test program to asses the planes' new handling characteristics with the leading edge cuffs that a friend (aircraft design engineer ) and I have installed - YAY !!!!!!!!!!!!
We'd really like a bit of input from those who have leading edge cuffs already fitted to their plane (Rebels or not) - as to what to expect / what the cuff did to :
1) The Centre of Gravity - ( did it move Fwd or Aft ? )
(my Neanderthal logic estimates that as the leading edge moves forward - the Centre of Pressure should move forward also (there's more wing chord / & area now) ... and therefore the C of G should move forward slightly - ( to keep in with the "most wings / planes will balance at about 1/3rd chord back from the Leading Edge" rule ) also ... Yes ?)
If that is so ..... then I reckon we should be REMOVING some of the 10Kgs of lead shot I have placed in the tailcone area ( to balance the "light weight" IO-320 with a NOT shortened firewall) ... Yes ???
2) The RANGE of C of G - (did it get bigger / smaller - or stay the same & move forward overall or aft overall)
3) Any salient points to keep an eye out for ?!?
AS always - your thoughts and opinions are gratefully received !
Biggus
541R
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David A. Ricker
Fall River, Nova Scotia
Canada
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