• Welcome aboard HomebuiltAirplanes.com, your destination for connecting with a thriving community of more than 10,000 active members, all passionate about home-built aviation. Dive into our comprehensive repository of knowledge, exchange technical insights, arrange get-togethers, and trade aircrafts/parts with like-minded enthusiasts. Unearth a wide-ranging collection of general and kit plane aviation subjects, enriched with engaging imagery, in-depth technical manuals, and rare archives.

    For a nominal fee of $99.99/year or $12.99/month, you can immerse yourself in this dynamic community and unparalleled treasure-trove of aviation knowledge.

    Embark on your journey now!

    Click Here to Become a Premium Member and Experience Homebuilt Airplanes to the Fullest!

Spar Layup Schedule

This site may earn a commission from merchant affiliate links, including eBay, Amazon, and others.

berridos

Well-Known Member
Joined
Oct 10, 2009
Messages
1,164
Location
madrid
Hi Everybody

Spar Construction.jpg

Enclosed the composite layup schedule for a C spar with poltruded carbon rods.
I have two questions.
Should i have some cloth layup between the sandwich core and the graphlite rods (gap in the graph)?
How long would you size the overlap between the outer shearweb and inner shearweb at the ends of the C?
Would you bond the core (Rohacell) and the rods with metacrilate or epoxy
Thx
 
Back
Top