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Greater than ever rates of climb in fighter aircraft like the new joint force achieve fighter - games


We know from studying aircraft like the F-8 Crusader, in which my dad had the fortunate to fly while in the US Navy stationed in Puerto Rico, that when the wind was off-center upward on the aircraft that it had a lower impersonation speed and much elevated opening rates of climb. At which point the wing came back to attitude and it was a pencil shaped rocket with wings. Now then let us take the newest discoveries in wind tunnels about life, weight, thrust and drag. We know that the reletive wind approaching on the base of the wings air force the aircraft up.

Well then if you have a thruster affected on top of the wing at the axis of gravity with the exhaust enforced outward, close to on the aircraft while the aircraft is positioned in a climb. This aircraft will for that reason be put in a location where the it is enforced into the family member wind more rapidly and earlier and that wind deflected off the base of the wing would force the aircraft upward at an incredible rate of climb not including appreciably using up any more fuel than a banner climb out. The rate of climb will be much nearer and the angle of climb very substantial.

I bring this up as we argue some of the NASA lifting bodies and other designs to fly into orbit or for trans-oceanic flights using the upper character or space to cut down the friction and augment the speed to hypersonic levels. We are doing comparable effects on the Arrive at Fighter, but those nozzels are faced down for vertical upstairs hallway and take off or exceptionally prohibited and fast STOL. If the wings can hold the amplified stress from the base of the aircraft aligned with reletive wind. Now then you can try this on a skateboard. Carrry a 4 X 8 sheet of plywood and when going down a hill tilt the plywood to a 45 grade angle and you will leave the bring down like a kite. If we have nozzel and directional thrust why not try it at the core of gravity on top of the wing forcing the exhaust apparent and back wards at the same angle of incidence to a horizontal plane.

You in fact do not even need to test this in a wind tunnel, for the reason that we by now know this will work. If you look at the chracteristics of the Concorde where the nose faces ahead and air is compulsory under the wings you can see the amplified competent use of the airfoil. The bigger force from the ram air under the wing is more than the total pooled army of lift from the differences amid low and high burden as the air makes it back to the trailing edge of the wing. Just some opinion on greater than ever the airborne characteristics of jet aircraft and directional thrust aircraft to augment all known characteristics of flight.

"Lance Winslow" - If you have innovative opinion and exceptional perspectives, come think with Lance; www. WorldThinkTank. net/wttbbs


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