Why do F-15E's engines have 10530kgf of thrust, instead of ~13200kgf?

except f18 it basically has no channel loss (only 0.6% or 51kgf)

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Capture d'écran 2025-04-27 202400
Capture d'écran 2025-04-27 202255

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yeah but gaijin seems to kinda make up channel loss percentages and all f15s have a weirdly high ~20-25% where most are 10-15%

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Isn’t it a straight shot to the engines?

idk, that isnt the only cause of channel losses though because they can be caused by intake not being large enough for engines ideal airflow but ive not seen anything suggesting that that is a big factor on f15

Opened up Eagle intakes are huge

I know, thats why I think its weird that f15 channel losses are so high

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Thanks for replying everyone

Gaijin’s source is they saw it in a dream

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Well. That’s very gaijin of them

This, IRL channel loss is a simple calc of the airflow required vs the inlet size and turbine intake size.

Gaijin is fully arbitrary in their choices with some engines like the TF34, which have literally no channel to have channel loss on, still suffering somehow.

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And what should i make out of this?

That there are many factors that contribute to installed thrust (what Gaijin calls “channel loss” for some reason)

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Mhm. And are these accurate for the F-15?

They affect all jet engines

yes we understand that, we just dont know where their numbers are and why they gave f15s higher than average channel losses

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6c6b50a4f48dbbf59b1986408e94d065

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It could be the manual provides data for installed thrust, which is where they got that number from. If not, a source would still be needed that disproves it.

ive looked through the publicly available f15e manual and I didnt see it

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image

Da yis, the authority on jet engine performance, any company in the Middle East.

Very funny that for some reason they think nozzles change on aircraft engines since the late 1970s, that stopped being a thing long ago since nozzles are included in nearly every single jet turbine that exists today, even civilian ducted turbofans.