Grayhawk,
Yes...
208/195 is only about 1.067 ratio.
However, changes
in speed with changes in prop efficiency is not
linear.
What you
are missing is that
speed (absent the details of the drag
polars) up in this range generally goes as about the cube root of power, or in this case,
thrust HP ( Thp = Bhp X
nProp) where nProp is the efficiency of the prop at the given
airspeed, RPM and Hp
loading.
Actually, one ought to use the TAS numbers, but
short of that:
So (208/195)^3 about = to 1.21 - - thus, my comment that the numbers reported
suggest about a 20% improvement in prop
efficiency.
Regards,
George
PS. Has anybody developed a set of
drag polars for a Lancair IV P ?