History post test result

creedo299

Epochal Historian
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?
 
Information removed, of the personal nature.

However kept in ,my p.m. box.

So you would have to hack, in order to get to see it.

I never belived in hacking, thought it was imoral.
 
If you want to talk about pistons, and conrods, check this.www.fpv.com.au
 
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