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[return to "The next steps for Airbus' big bet on open rotor engines"]
1. direwo+V71[view] [source] 2026-02-03 20:10:57
>>CGMthr+(OP)
Is this not... a propeller? A turboprop engine?
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2. idontw+ph1[view] [source] 2026-02-03 20:55:02
>>direwo+V71
I’m not an expert but I think the distinction is that the blade tips in these reach supersonic speeds like in turbofans. That is a hard problem to fix because you don’t have the duct to contain the noise and catch the blades if one were to break.
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3. JumpCr+aN1[view] [source] 2026-02-03 23:45:12
>>idontw+ph1
> the distinction is that the blade tips in these reach supersonic speeds like in turbofans

Commercial engines are not designed to have anything to supersonic.

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4. idontw+sQ1[view] [source] 2026-02-04 00:03:53
>>JumpCr+aN1
https://aviation.stackexchange.com/questions/22316/why-do-tu...
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5. JumpCr+PW1[view] [source] 2026-02-04 00:42:59
>>idontw+sQ1
Sorry, you’re correct. You want to avoid supersonic tips as much as possible.

Modern turbofans permit supersonic tips during high-thrust regimes. (Part of the work in these new designs is releasing that constraint since those supersonic tips are a bastard.) It’s something sought to be avoided. But not at all costs at all times.

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