New thread
In last thread 4, i happened to post some query about JF-17, but as that thread got closed, i am posting it again here.
Few questions regarding usage of composite in JF-17.
I have read that Raptor has 25% carbon composite while 38% Titanium alloy (by weight).
In any older plane the decision to increase composite material ratio is taken by considering the cost-benefit analysis. If by increasing Carbon composite the TWR, operational life, Radar signature factors are significantly improve, only then Carbon composites are added.
Is there any study in this regard for JF-17 has been carried out or being under study right now?
How much Chinese have mastered the technology of carbon composites and its modeling/tooling?
And Which portion of JF-17 is Titanium alloy?