History post test result
Modifications without any argument.
Sample test engine, Titan wrecked aircraft engine, horizontally opposed six cylinder engine, being carried to rebuilder.
Area of a piston, was a little more than a tin fruit juice can.
Modifications:The number of cylinders placed,. is in a radial fashion around a central hub.
The exhaust impart is jacketed, to be pumped back onto the cylinders themselves.
Electrical output, is not determined at this time, to be added to a dilution of energy principles around those cylinders?
JET ENGINES:The interior airflow passage of this jet engine, is hardened so that a uniform plasma sheath, may be installed throughout the entire engine.
Ionize plasma, injected into the ion air fuel mixture flow, regulated a uniform thrust.
DRAG COEFFICIENTS Not presented in modulace, working CAD model, via mail simulation, of air stand, as opposed to air jet velocities along a straight line.
There is no barometer nor air density simulation mailed, which shows input of any static or moving engine, over a straight-line course?
One figures if this is not offered or any changed offered in course curriculum, then why bother?
