The Grumman forward swept wing X-29 experimental aircraft was adapted from an existing F-5A airframe. Because of the inherent aerodynamic instability of the forward swept wing design (think of an arrow shot backwards) a computerized fly by wire control system was necessary. The advantage of this design as opposed to conventional back swept wings were higher lift-to-drag ratio, higher capacity in dogfight maneuvers, higher range at subsonic speed, improved stall resistance and anti-spin characteristics, improved stability at high angles of attack, a lower minimum flight speed and, a shorter take-off and landing distance but, all of this came with a price of inherent instability and much higher drag at near supersonic speeds. The forward swept wings, with movable canards, gave pilots excellent control response at up to 45 degrees angle of attack.
Because of the availability of F-5s and advances in low cost computer control systems Turkish Aerospace Industries has considered upgrading some existing TuAf F-5s with X-29 designs.
Tags: x29 forward swept wing