Hi guys
I just realised that the fact that the outer wing spars are narrower by the
thickness of the two W.A.F's. This will account for the outer spars being
about1.3mm less in total height due to the fact that they make contact with
the skin a little further aft than the centre spars (leading edg
Dene: Hello
I think you will find that the CG remains very close to where it was
originally. What will move back is your center of lift. The CG may
still be within limits but you would need to check. Moving the Center of
lift rearward would increase the work load of your horizontal stabilizer
aft.com
- Original Message -
From: "francis fenlason"
To: "'KRnet'"
Sent: Monday, January 19, 2004 4:05 PM
Subject: RE: KR>rear spar HELP
Hi guys
According to my calcs, the centre of the rear spar is not dead on 75% chord.
It is on 75.27%. Using compufoil I placed the rear spar at this location and
set it to distended depth. I then worked out that the tallest part of the
spar would be at 74.088% chord. This also happens to be the lea
Dene,
My approach was to get the center forward spar bonded in place
and then use the 48 inch ribs to locate and bond the rear center
spar. It has to be mounted inside the wing shape and the ribs
will tell you where that is. Using Mark Langford's ribs with the
humps should make it a "no braine
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