It looks like you're using an Ad Blocker.
Please white-list or disable AboveTopSecret.com in your ad-blocking tool.
Thank you.
Some features of ATS will be disabled while you continue to use an ad-blocker.
originally posted by: Zaphod58
a reply to: Barnalby
You didn't miss much with the 757. Now the 767-400, that's a nice ride.
originally posted by: Zaphod58
a reply to: Sammamishman
They'll put stiffeners where necessary.
originally posted by: Sammamishman
a reply to: Barnalby
I'm not sure it would flex that noticeably over the length of the fuselage. Aluminum doesn't have anywhere near the malleability of wood or composites depending on the ingredients. If it was flexing to an extreme, that it could be noticed by passengers, I don't think it would hold up very long to the stresses of flight. In addition, the interior panels might be able to cover or deaden the observability of what ever flex might exist in the structure.
I'd like to know what structures Boeing might have to add to strengthen the fuselage lengthwise or if the current design already has the strength built in to take the added stress.