| ▲ | Galxeagle 3 hours ago |
| Not clear to me from the article - what's the different between an 'open rotor' engine and a turboprop (https://en.wikipedia.org/wiki/Turboprop)? At face value, both seem to be jet engines with propellers used on single-aisle planes? |
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| ▲ | kdaker 3 hours ago | parent [-] |
| There is still a jet stream coming out of the engine propelling the aircraft. Unlike a turboprop where only the propellor generates thrust. |
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| ▲ | JumpCrisscross 3 hours ago | parent [-] | | > Unlike a turboprop where only the propellor generates thrust Each of turbojets, turboprops and turbofans generate thrust with exhaust. | | |
| ▲ | shawn_w 2 hours ago | parent [-] | | Turboprops have no meaningful thrust component from the exhaust. | | |
| ▲ | ahartmetz an hour ago | parent [-] | | Almost. Wikipedia says 10%, which is kinda meaningful but really not much. Even some piston engines (like in WW2 fighters) get 2% or so from exhaust. |
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