May 01, 2007, 09:02 PM
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st. paul, mn.
Joined Jan 2007
2,675 Posts
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ABSOLUTELY GANG!!
without using all that engineering terms, here we go;
As a Canard uses 100% of horizontal area for lift, we will use percents for the base of calculations with a sketch as reference;
1) Main wing square inches=XX
2)Main wing quarter chord =sub(little) c
3) Canard square inches= XX(canard)
4)Canard quarter chord= subc
5Distance of mounting =Length using quarter chord locations;
NOTE- I personnally like my spars to be perpendicular to Length, at the thick point of foils, and I use the (Spar)- wing rod for distance references
just using math, we will assume a main wing of 500 sq" and canard of125 sq"
main plus canard =625 sq"
Length of mounting we will use 25"
To get our Neutral point, we go length multiplied by Mainwing-25x500=12,500(
)divided by total sq."= 20 "
Still with me? the length 20 inches is our NEUTRAL POINT from the Canard's quarter chord towards the main wing Length, which would be a distance forward of the Main Wing leading edge
NOW THE CRITICAL PART
The STATIC MARGIN= ( ENVELOPE) this will establish the aircrafts' stability of flight.
for the most forward Center of Gravity, we will use 15%, and for flying "the ragged edge" we will use 10%
We have established that 20 inches from Canard Quarter chord is the neutral point,
Now we need the (bar sub C) which is the proper termfor the Mean Aerodynamic Chord= MAC which is average chord, being square inches divided by span.
We haven't established a span in our calculations, yet, so we will go with 50 inch span, for math, we are using a rectangular wing, 500 sq" divided by span of 50" gives a MAC of 10 "
Now the STATIC MARGIN'S calculations are 15% of 10" MAC, PLUS the 20"= 21.5", Right?? actually no.
AS the neutral point of aircraft would be considered ZERO, forward of neutral point
would now be calculated in the negative, meaning the 1.5" is subrtacted from our 20" Neutral Point=18.5" and at 10%, 19 inches from Canard's Quarter Chord.
This would be the ENVELOPE
Did I come across clear as mud? Obviously, I willneed to update/ edit future details, in the morning -Igotta goto work, now
Johnny
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