disagree on the jury being out on 30 years. Its very easy to simulate 30 years of cycles. Ive done it on a few aircraft now. CF doesn't degrade like AL does due to fatigue as long as you dont pass certain limits it does have an infinite life spangilgen wrote:Of course, air is a "fluid". But I reiterate that in the Americas Cup boats, over the last few years, the builders have been borrowing from F1 techniques and design. You wont find many large container ships using slotted wings as sails.Just_a_fan wrote:The early aero stuff was often carried out by guys who moved over from hydrodynamics work such as ship designing.
Indeed, I chatted to a chap running a wind tunnel a few years ago. He'd started in F1 with McLaren (if I remember correctly) having been working on in marine design originally.
I found the comment earlier in the thread, about F1 helping boat design, rather funny in view of this...
White blue, The dreamliner is using cf for its body and wings, something that was not tried before, other than in small jets. Already there have been serious problems with strength of attachment between wings and body. Unfortunately, nobody is sure if cf has a finite life. As aircraft have to suffer the stresses of thousands of cycles, they need to be sure that aircraft will last 30+ years. The jury is still out on that one.
Set up a new thread with a link to this one.WhiteBlue wrote:It takes a moderator to do that retrospectively. And you can only pick a limited number of votes like 10.
The B2 isn't a small aircraft. The maximum take of weight is more than 160 metric tons and the wing area is more than 500 square meters.gilgen wrote:White blue, The dreamliner is using cf for its body and wings, something that was not tried before, other than in small jets.
And it costs more than an aircraft carrier to produce one B2 (think $billions). F1 techniques with cf have allowed the production cost using those materials to continue to decrease to a level where they are almost affordable.WhiteBlue wrote:
The B2 isn't a small aircraft. The maximum take of weight is more than 160 metric tons and the wing area is more than 500 square meters.
The point was which industry pioneered the use of carbon fibre composites in the first place and developed the manufacturing technologies, simulation methods and design principles. I don't think anybody can say with some degree of honesty that F1 did more than the the aerospace industry and that aerospace at any time had a need to learn much from F1 in terms of fibre composite materials. In the context of this thread one has to say that F1 did a me too.volarchico wrote:And it costs more than an aircraft carrier to produce one B2 (think $billions). F1 techniques with cf have allowed the production cost using those materials to continue to decrease to a level where they are almost affordable.WhiteBlue wrote:
The B2 isn't a small aircraft. The maximum take of weight is more than 160 metric tons and the wing area is more than 500 square meters.