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In a message dated 8/20/05 8:23:31 AM Pacific Daylight Time,
[EMAIL PROTECTED] writes:
I have in the past bagged CF to existing spruce spars, but have never Barry,
Nearly all of the wing failures are in compression,
meaning the top of the wing fails first. In extreme cases, sections of the
wing near the root will be missing entirely (turned to dust) from the force of
the failure.
Therefore it makes sense to stiffen the upper spar
a bit more than the lower. In the past I have used .014 pre-preg for the
upper spar and .007 for the lower. As you observed CF is better in
extension than compression. Ideally, placing the CF in the middle of the
upper spar would provide great strength, but placing it under the spar and on
top of the shear web (and ribs) should suffice.
Look forward to seeing your new Challenger. I
too have one in a box and am searching the web for a barrel of patience before I
start building it.
Don
Richmond
San Diego, CA [EMAIL PROTECTED] www.hilaunch.com |
- Re: [RCSE] CF on spruce spars - on the right track Hilaunch

