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take-off thrust

take-off thrust

take-off thrust

(OP)
Hi, I'm working on a conceptual design of a civil transport aircraft. I've some troubles estimating take-off thrust reduction vs speed for high by-pass engine. I'd appreciate any suggestion or reference books. Thanks.

RE: take-off thrust

Takeoff thrust is anywhere from 30,000-50,000 lbs typically depending on the engine.

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