Increasing Rates of Climb in Fighter Aircraft Like the New Joint force Strike Fighter

We know from studying aircraft like the F-8doing similar things on the Strike Fighter, but those
Crusader, in which my dad had the fortunate to flynozzels are faced down for vertical landing and take
while in the US Navy stationed in Puerto Rico, thatoff or extremely controlled and fast STOL. If the
when the wind was tilted upward on the aircraft thatwings can hold the increased stress from the bottom
it had a lower takeoff speed and much higher initialof the aircraft against reletive wind. Now then you
rates of climb. At which point the wing came back tocan try this on a skateboard. Carrry a 4 X 8 sheet of
position and it was a pencil shaped rocket with wings.plywood and when going down a hill tilt the plywood
Now then let us take the newest discoveries in windto a 45 degree angle and you will leave the ground
tunnels about life, weight, thrust and drag. We knowlike a kite. If we have nozzel and directional thrust
that the reletive wind pushing on the bottom of thewhy not try it at the center of gravity on top of the
wings forces the aircraft up.Well then if you have awing forcing the exhaust outward and back wards at
thruster forced on top of the wing at the center ofthe same angle of incidence to a horizontal plane.You
gravity with the exhaust forced outward, pushing onactually do not even need to test this in a wind
the aircraft while the aircraft is positioned in a climb.tunnel, because we already know this will work. If
This aircraft will therefore be put in a situation whereyou look at the chracteristics of the Concorde where
the it is forced into the relative wind faster andthe nose faces forward and air is forced under the
faster and that wind deflected off the bottom ofwings you can see the increased efficient use of the
the wing would force the aircraft upward at anairfoil. The increased leverage from the ram air under
incredible rate of climb without significantly using upthe wing is more than the total combined forces of
any more fuel than a standard climb out. The rate oflift from the differences between low and high
climb will be much faster and the angle of climb verypressure as the air makes it back to the trailing edge
substantial.I bring this up as we discuss some of theof the wing. Just some thoughts on increasing the
NASA lifting bodies and other designs to fly into orbitflying characteristics of jet aircraft and directional
or for trans-oceanic flights using the upperthrust aircraft to maximize all known characteristics
atmosphere or space to reduce the friction andof flight.
increase the speed to hypersonic levels. We are