• 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!

Composite Design Practices

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

Aerowerx

Well-Known Member
Joined
Dec 1, 2011
Messages
6,097
Location
Marion, Ohio
I just found this paper on Composite Design Practices.

PDF page 4 contains these statements:

A 0 degree/90 degree stacking. This arrangement bends under pure tension because the modulus-weighted centroid is not coincident with the geometric centroid, resulting in an offset load path.



sketches show how simple loads result in unusual deformations because of coupling action. With balance and symmetry present, these effects disappear


(arrgh! can't remove indent for some reason. Anyway...)

I thought these were interesting pictures. The 0/90 stack is shown bending in only one direction. It leads me to believe that a 0/90 stack is best for landing gear legs???

Edit: I think theoretical concepts are easier to grasp when there is a clear picture.

 
Back
Top