KC135DELTA
Well-Known Member
- Joined
- Aug 1, 2006
- Messages
- 112
Hello,
I was running a simple (by my standards) design through my head for a high performance semi-aerobatic aircraft that utilizes a turbo normalized IO-540. When conducting rapid descents from the flight levels how can shock cooling be addressed? I'm sure there is some sort of a solution developed by now?
onder:
Thanks, any input welcome
I was running a simple (by my standards) design through my head for a high performance semi-aerobatic aircraft that utilizes a turbo normalized IO-540. When conducting rapid descents from the flight levels how can shock cooling be addressed? I'm sure there is some sort of a solution developed by now?
onder:Thanks, any input welcome
