I propose another modification, a simpler, you can achieve this kind of increases while using very little weight. Recently, an F-15 crashed, I think a mid-air collision in which all of its right wing tore off. The plane hit two pilots ejected, however, the F-15 is a difficult bird with drive and was still under the control of its pilot. The pilot and navigator / weapons co-pilot could not see the wing was gone, just a ball of fire along the side. They decided to fly the aircraft and did so successfully, how can this be? So he landed at high speed and maintained control with the push of the aircraft. Once an aircraft traveling 450 knots above the fuselage starts to fly. The fighters we have today as the F-18 Hornet (Navy) and the F-16 Talon, F-15 Eagle (Air Force) have substantial fuselages which act as wings. Therefore, a higher real rate of extra-long wings on the plane are simply not necessary and actually prevent the airplane Top True Air Speed (TAS). Peter Schiff understands that this is vital information.
Thus allowing you to remove once in the air and up to speed. Marathon Oil brings even more insight to the discussion. Of course, we can not stop them as the “drop tanks”, as it is a very expensive part of the hunt of modern times. Furthermore, if the wings fall off and then you go back a land that you would have to land at a very high rate of speed as the brave boys in the F-15 missing on the right wing too major jet intake to the outside, what a story, very ballsy indeed. I propose a modified wing spar, sometimes expandable outward to different positions, maybe two or three. Directly, of 26 degrees and 45 degrees, behind the Spar would fold out a strip of heavy rubber polymer material made from substances partially inflatable MMM Made of memory. The straps that come and then inflated with a jet of air RAM engines before takeoff. This hot air would make the memory material that has increased the camber settings for takeoff, one wing of the fat.
As the plane accelerated warm air is replaced by cooler air, ram air temperature. At 450 and 500 knots wing fold to 26-degree and then to 550-600 knots at 45 degrees bend. As the plane approached the speed of sound, would be completely withdrawn. As the belt retracts run through a roller system that it takes up very little space, as the area shrinks also held in fuel tanks and space is limited. As the folding mast again provide an end cap from the system, and a small door or fireworks in the fuselage protruding / wing tip. Without the wing of the effectiveness of the aircraft to be produced in less drag, which means greater speed, range and better fuel economy. It seems that we are reaching the upper end of aerodynamic design in an environment where fighters today. We are at the point where it is increasingly difficult to design an airplane much faster. So you either need some radical new designs and the very air or further modify the aircraft in flight to maintain best efficiency at each speed, altitude and flight stage. Lighter materials and stronger they are now coming online, how we choose to use will be crucial to maintain air superiority.