DarrenW
Staff Sergeant
We have at least 2 variables that contribute to the difference in cruise speed vs the power used.
1. may be the efficiency of the respective propellers at cruise speed/altitude.
2. maybe a difference in exhaust thrust. However this may not be great. The P-47 gets darn little (I think?)
But the amount the F6F gets at cruise speeds may not be a lot either. At 36in and 2300rpm the engine is moving about 57% the amount of air it is at 54in and 2700rpm and since exhaust thrust is mass times velocity the fact that you are running lean means less fuel per pound of air.
F6F exhaust is better than than an early F4U but not as a good as a V-12
View attachment 503723
That middle pipe in the upper 3 may do pretty good but the top pipe doesn't look so good. The longer the pipe and the more/sharper bends the lower the exhaust gas velocity.
An engine running 54in of boost in the cylinders will have higher pressure/velocity gas leaving the exhaust ports than one running 36 in of boost.
Trying to compare a 1200hp V-12 running at 48in boost to a large radial loafing at 1200hp with 32-36in of boost may not be accurate.
Awesome stuff as usual SR6. I'm going to need a little time to digest what you said so I understand it completely...