Wing weighting
Anthony Romano
anthonyr105 at hotmail.com
Sun Aug 1 09:55:34 AKDT 2004
Richard
I understand your situation. Sometimes bad things happen. Great to see the
perserverance.
http://f1.pg.photos.yahoo.com/ph/nypattern/album?.dir=/fd57&.src=ph&store=&prodid=&.done=http%3a//f1.pg.photos.yahoo.com/ph/nypattern/my_photos
take a peak at the link
Anthony
>From: "Richard Strickland" <richard.s at allied-callaway.com>
>Reply-To: discussion at nsrca.org
>To: "NSRCA" <discussion at nsrca.org>
>Subject: Wing weighting
>Date: Sat, 31 Jul 2004 11:58:04 -0500
>
>Gentlemen,
>
>I made a large error a few weeks ago and totaled the first Temptation. Got
>the second one done and had problems with the engine and it had to go back.
> Wife had gone to California to help her Aunt move--So I'm home alone,
>have to come home after work to let the dog out and the field is too far
>away to practice after that with the old trusty OMS. What to do--what to
>do.... Got to looking at the "totaled" airplane and started tacking pieces
>back together--got to thinking hmmm--this might actually become an airplane
>again--called Lee and asked him for some cores and a chin cowl--told him I
>had two weeks of guilt free building time and would he send a set. Well,
>it was right before the Nats and it didn't happen--understandably.
>
>So I had this severely crunched left wing panel--really NOT
>salvageable--now with all kinds of foam voids--wing socket knocked loose
>and should have pitched it--but I didn't. I did some judicious goobering
>(read HEAVY) of epoxy and foam as best I could, lined up the wing halves
>back in the shucks with the wing tube--weighted them, said a little prayer
>and let 'em set. Well, at least it started looking like a wing. The socket
>was still a little wobbly and I still had to graft about 25% of the
>crunched nose of it on and again--probably should've pitched it. But
>nooo.... I cut a couple lite-ply spars, cut grooves for them from the
>bottom side up to the socket sides and glued those in--back in the shucks.
>Still didn't like the rigidity--so I did a couple spars on the top with a
>contoured cross partial rib boxing the socket, grafted foam, resheeted as
>needed, blah, blah, yada, yada... Could have done a set in this time. Got
>the new cores yesterday.
>
>Here's the Question: Since I've added about 2.5-3 oz to the panel with the
>average about 30% out in span; would I add a similar amount of weight on
>the other at roughly the same spot or LESS weight toward the end? You
>know--levers, arms and all that.... I'll fly it as is and see how it
>reacts. You don't have to tell me that I need to build another
>panel--that's a given. Having an extra set of heavier panels around here in
>the spring wind may not necessarily be a bad thing. It started out at 10
>lbs.-7ozs.
>
>Thanks,
> Richard
_________________________________________________________________
Dont just search. Find. Check out the new MSN Search!
http://search.msn.click-url.com/go/onm00200636ave/direct/01/
=====================================
# To be removed from this list, go to http://www.nsrca.org/discussionA.htm
and follow the instructions.
More information about the NSRCA-discussion
mailing list