JF-17 THUNDER/ FC-1

1. Aerodynamic Configuration

Bifurcated side air inlet.
New wing with ability of high angle of attack
Leading edge maneuvering flap
Trailing edge...

Related Keywords

China ,France ,French ,Chinese , ,Chinese National Military Specification ,Martin Baker ,Landing Gear ,Safe Escape System ,Environment Control System ,Designed Flight Control ,Electrical Power Supply System ,Main System Failure ,Fatigue Life ,