Post by kimPost by William H. ShueyFWIW The part of the P-38 story that I would like to see investigated
is why there was no attempt to fit the P-38 with the Merlin 60 series in
place of the Allison/Westinghouse supercharger/inter cooler combination.
Swapping a singlestage blower equipped Merlin in a P-40F showed
little improvement over the singlestage Allison.
Post by kimPost by William H. ShueyTwo 60 series Merlins with their internal supercharger would have
It wasn't internal to the engineblock, but coupled.The disadvantage
of the Allison was it had an Integral blower, which made it
difficult to add an extra gearbox onto it, but no effect on adding
Turbos. This wasn't changed on Allisons till late in the war.
More on this later.
Post by kimPost by William H. Shueyresulted in a weight saving and more space for gas. It was never
attempted, and as far as I know was never investigated by Lockheed. Why?
Turbochargers could be lighter than a gear driven multistage,
multispeed blower, but take up more volume for ducting. This advantage
is lessened if the supercharged Merlin was fitted with an Aftercooler,
that cooled the compressed air before it got to the intake manifold
Allisons could be Intercooled, the airtemp reduced between
turbo and internal blower, but not aftercooled easily.
Post by kimI'm guessing it has to do with the cooling arrangements. The P-38 was
essentially a flying radiator. It might have been more difficult to cool a
pair of Merlins than a pair of Allisons? Just guessing.
For a given HP output, an engine will make similar amount of waste
heat, needing cooling from oil and glycol to prevent the engine
from melting down. The two engines had similar displacements
and compression ratios, and so for the same power levels,
would make similar amounts of BTUs to be cooled
All forms of Boost takes HP to run the compressor.
A Merlin might need 150HP off the crankshaft to get to 1500HP,
while the Allison gets that from the free exhaust to get to 1500HP.
The gear setup needs to make 850HP worth of max boost, while the
Turbo only 700 to get to 1500HP total, given that both engines made
about 7-800HP at Sealevel without any extra boost/water injection/etc
At 30,000 feet, either engine would make about 1/3rds its base sealevel
HP output, about 300HP. It was easier for the Turbo to make up the
extra boost needed to keep power levels up in very thin air, the
Supercharger is starting to eat a large percentage of the engines
output,just to run the supercharger, let alone provide boost to
increase the power level
This is why the USAAF Bombers and P-38 and P-47 had Turbos, V.high
altitude performance.
Postwar, the 'Twin Mustang' used Allison power, but with a two stage
blower, and was similar to the Merlin in HP output at Altitude.
Also postwar, hydroplane racing showed the Allison did well vs
Merlin powered boats.
The engines were really pretty similar. Its just the Merlin
had a two stage blower, vs the Allison single stage, that gave the
Merlin its advantage.
The 'Ultimate Allison' near 3000HP using Turbocompounding,
was cut short by tubojets.
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mike
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