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1. Galxea+(OP)[view] [source] 2026-02-03 23:18:48
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?
replies(1): >>kdaker+n1
2. kdaker+n1[view] [source] 2026-02-03 23:27:01
>>Galxea+(OP)
There is still a jet stream coming out of the engine propelling the aircraft. Unlike a turboprop where only the propellor generates thrust.
replies(1): >>JumpCr+K2
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3. JumpCr+K2[view] [source] [discussion] 2026-02-03 23:34:28
>>kdaker+n1
> Unlike a turboprop where only the propellor generates thrust

Each of turbojets, turboprops and turbofans generate thrust with exhaust.

replies(1): >>shawn_+d8
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4. shawn_+d8[view] [source] [discussion] 2026-02-04 00:03:01
>>JumpCr+K2
Turboprops have no meaningful thrust component from the exhaust.
replies(1): >>ahartm+Bk
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5. ahartm+Bk[view] [source] [discussion] 2026-02-04 01:20:56
>>shawn_+d8
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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