• 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!

Shear flow in wing box and single strut

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

rapidshot

Well-Known Member
Joined
Jan 31, 2015
Messages
69
Location
ankara
Hi all,

I have been thinking on the subject for a while but couldn’t make an approach for hand calculations,

Any recommendations are welcome, how does a single strut attached to front spar affect the shear flow in the box due to torsion,

Do you think that shifting the elastic axis linearly from wing tip to strut attachment point is a good approach?

Thank you,
 
Last edited:
Back
Top