I have an IO-360, parallel valve with a vertical induction. Propeller is a Whirlwind 200RV.
I usually cruise LOP at 9500' to 11,500' and see 171kts TAS if I am solo. Fuel flow is just under 8gph. RPM is 2400. If I'm near gross that speed will drop to 168-169 kts TAS.
If I cruise ROP at the same altitudes and RPM, I will get ~176kts but fuel burn is significantly higher.
At 8500' density altitude, WOT, 100 degrees ROP, 2700 RPM I see 181kts TAS. I've only done that once or twice as fuel burn is horrific, and it's hard to get to 8500' density altitude around here without running into the ground.
I don't have much experience at lower altitudes, you'll have to get that info from a flatlander.
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