I have not got trough the links provided earlier so sorry if I am repeating things you already knew.swordfish wrote:I allready know the basics, lighter, stronger, possible indefinate lifespan if used within the manufacturing tolerances but i was looking for actual facts and data to back up what i hypothesise to be correct.
Information about cost as well would be good. I've read that carbon materials can be relativly cheap now and manufacturing cost can be lower than making metal components but have any teams ever offically published a cost ratio between the two.
Joining composite parts, as well as composite-metal connections (you have metallic joints on both ends of the wishbone), is not so simple. Partially due the fact composites do not like "localized" forces.
Maybe it's not a big deal in case of wishbones (my experience with them is limited to the fact I knew how they look like), I am talking from the aviation perspective. As an example - one of "Dreamliner" prototypes was grounded few weeks ago due issues with joints and fasteners connecting wings and fuselage.