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by gjrq
190 days ago
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Oh come on, what is this crap? Absolutely no thermal efficiency numbers or anything else you could use to validate any claims. Especially if you are claiming that an aero-derived turbine is somehow going to be better than a purpose-built unit. The "supersonic engines are better because they are designed to operate at hotter temperatures" argument is particularly insane: turbine efficiency is driven by turbine inlet temperature (already 3000ish C), not ambient temperature. I suppose it's only right that VCs are going to get scammed by LLM slop. |
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For all their discussion of high temperature operation, it seems the only advantage at the end of the day is to eliminate water consumption in cooling. I question if that's really so valuable?