On Tue, 6 Jul 2004 02:21:23 +0000 (UTC), Louis Capdeboscq
Post by Jim SpeiserI'm researching an aspect of the Battle of Britain, specifically exactly how
the UK came into possession of the 100-octane fuel that allowed the
Sptifires to climb higher than the Me-109s.
Higher octane fuel did not allow Spitfires to climb higher than the
Bf109E's that they flew against during the Battle of Britain. In
fact, many historians give the edge to the 109 in high altitude
capability.
What the high octane did do for the engine was allow the Rolls Royce
engineers to introduce a more efficient supercharger for the Merlin
that forced more air and fuel into the intake manifold than the
version used in the Mk1's.
Horsepower production is a matter of fuel/air + ignition + compression
+ rpm. Increase any one of those factors (except for ignition which
only needed to ignite the mixture at the proper time) and you get more
power, up to a point. At some point, you can exceed the ability of
the engine to stay together, or the fuel to burn properly, or the
ignition to ignite properly. The point is, none of the engines of
that era had reached their ultimate development yet. The Merlin is
now producing in excess of 3,000 horsepower for races at Reno and it's
basically the same engine, albeit with some compression and
supercharger changes and some unholy fuel mixtures.
The Rolls Royce engineers were told that a higher octane fuel was
being developed, and modified the Merlin to make use of it by revising
the amount of fuel and air that got packed into the intake manifold.
They could do this because they knew that the higher octane fuel would
resist detonation that would otherwise have occured with the higher
manifold pressures being run in the engine. They managed this in
large part by revising the supercharger, allowing it to increase it's
compression ratio.
So what does this give you? It gives you an engine that, in the exact
same airframe, now produced more power. Coinciding with the higher
powered engine was the addition of a three bladed variable pitch
propeller which allowed the pilot to use the full throttle without
worrying about overspeeding the engine: he could select maximum rpm
and push the throttle to full military power and know that the engine
would stay bolted together, even in a dive.
But this did not necessarily give it a higher ceiling than the Bf109,
nor did it give it a better performance at extremely high altitude.
This was because even though the new supercharger was superior to the
older one, there were still limits to what it could do and the
Messerschmitt was optimized for better performance at higher altitude
than the Spitfire. Luckily for the Spitfires, most of the combat
occured at less than the absolute maximum altitude the fighters were
capable of. At medium high altitudes, from 18 to 20,000 feet, the
Spitfire could hold it's own against the Bf109E.
Corky Scott
PS, simply using 100 octane fuel in an engine optimized for 87 octane,
with no changes, would have done nothing for engine performance. The
only way to increase performance is to increase either rpm or
compression. Since there were also physical limits as to how fast
props could turn, that left only compression (or cubic inches) as the
method for increasing performance. I take that back, the engineers
could have revised the ratio of the gear reduction unit that turned
the prop thus allowing higher engine rpm without increasing the
maximum speed of the propeller.