• 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!

Modulus of Rupture

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

Aerowerx

Well-Known Member
Joined
Dec 1, 2011
Messages
6,101
Location
Marion, Ohio
I want to make sure I have the correct understanding of this.

As I understand it, if you have a wood beam, supported at both ends, and apply a downward force at the mid point, when the force reaches the modulus of rupture the beam will fail. I guess it is roughly equivalent to the Elastic Limit of a metal.

If you use Hickory, for example, it has a modulus of rupture of 20,200 psi, and is one of the strongest hardwoods. So, if you have a beam with a 1 inch by 1 inch cross section, it will support up to 20,200 pounds before failure? Seems incredible, doesn't it?

Yes, I know that is an average value (or maximum value?), but still....

Of course, it may bend a long time before it actually fails. Maybe that is the limitation instead of the Modulus of Rupture.
 
Back
Top