Recip Turbo – Propeller efficiency?
Asked by: william0203usa 989 views Aerodynamics, Aircraft Systems, Flight Instructor
A C206 normally aspirated vs a turbo, both have 3 bladed props, 80"props that have an adjustable pitch from 12º to 27º.
At 14,000 feet, the 206 normally aspirated will have a lower prop pitch angle compared to a turbo 206 at 14,000? Obviously, the turbo can hold sea level to about 22,000, whereas the non-aspirated at 14,000 lost most of its power. What are the blade angles on this comparison?
I'm trying to understand how the same propeller can convert 285HP to useful torque at 14,000 compared to a normally aspirated producing 150hp. Is it all about pitch angles varying to "absorb" the extra torque?
Thanks
The following terms have been auto-detected the question above and any answers or discussion provided. Click on a term to see its definition from the Dauntless Aviation JargonBuster Glossary.