Originally Posted by Coheed
The other truth is the fact that the higher the turbine speed, the more backpressure. This is something that seems to be overlooked.
Awesome point. The exhaust side is affected as well. Very much over looked. I didn't even mention it, and it is very important. Good work.The other truth is the fact that the higher the turbine speed, the more backpressure. This is something that seems to be overlooked.
Originally Posted by Coheed
Now let’s go into the other workings of the engine. Higher boost is not the cure-all for high altitude engines. More boost will lead to more engine blow-by.
This makes sense as blow-by will increase as pressure in the crankcase decreases due to altitude. The odds of boost leaks would increase too I'd bet.Now let’s go into the other workings of the engine. Higher boost is not the cure-all for high altitude engines. More boost will lead to more engine blow-by.
Originally Posted by Coheed
Having a higher PR means the air is being compressed more, regardless of boost pressure. Even if boost is 2.2psi lower at high alt than sea level, the PR will still be higher. The more the air is compressed, the more heat is produced. The more heat, the more volume, the less dense the air is.
There's the meat of the argument again right there. Very well said.Having a higher PR means the air is being compressed more, regardless of boost pressure. Even if boost is 2.2psi lower at high alt than sea level, the PR will still be higher. The more the air is compressed, the more heat is produced. The more heat, the more volume, the less dense the air is.
Now your beard and plaid flannel are really shining through here. WTF less oxygen concentration at altitude? Makes sense, but I never thought about it. It's time to move to the coast man!