I saw that webpage, but it didn't quote anything, nor give any form of
justification.

Brent gave one, that perhaps was peak power at the end of ascent,
but it still doesn't sound quite right to me. Once an aeroplane is
airborne and landing gear is retracted, maximum thrust is no longer
needed.

I'm thinking that the velocity factor needed to compute maximum power
ought to perhaps be exhaust gas velocity anyway. It seems likely to me
that aircraft engines should be able to increase exhaust velocity and
correspondingly reduce thrust as velocity increases, keeping power
constant (much like gears in a car do).



On Fri, Jul 11, 2014 at 01:34:17PM -0400, John Clark wrote:
> On Thu, Jul 10, 2014 at 7:42 PM, Russell Standish <li...@hpcoders.com.au>
> wrote:
> 
> >
> > > I wonder where the 140MW factoid comes from?
> >
> 
> http://en.wikipedia.org/wiki/Orders_of_magnitude_%28power%29
> 
>   John K Clark
> 
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