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