OT....I knew you couldnt read...and now you proved it again...
205 hp/135 tq @6.5 psi on 87 octane @ 8200-8400 rpm
230 hp/155 tq @ 7.5 psi on 92-94 octane @ 8200-8400 rpm
427 hp/275 tq @ 22 psi on 120 octane @ 8200-8400 rpm
bone stock motors..NO internal work done...see ya at the top...BJ
Not to pick nits, but OT is closer to reality for altitude riding than it appears.
I have always had a problem with using boost to express hp when the baseline altitude changes. Aircraft, for instance use inches of mercury at the manifold pressure station, in short manifold pressure.
Sea level has 30" of manifold pressure or about 15 lbs of pressure outside.
Dynotech is at an altitude of ~ 1000' agl. There is 28" of manifold pressure there.
At 10,000 feet there is about 20" (10psi) of manifold pressure outside.
Now take the 230 hp power point at sea level /30" of MP add 7.5 lbs of boost / 15" of manifold pressure and at 45" of manifold pressure, it sounds like this motor makes about 230 hp.
Take that same motor up to 10,000 feet where there is a starting point of 10 psi or 20 inches of manifold pressure available, the motor needs to see a total of 45" to make its power, so the turbo needs to make 25" of manifold pressure or 12.5 lbs of boost to make that 230 hp.
Dunno if OT was doing his math this way or just shootin from the hip for the riding he does in the west/Wyoming. But technically he is right.
Like I said, I like the manifold pressure in inches method better, it brings everyone closer to speaking the same language. To bad everyone is stuck on the "Pounds of boost thing....."