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In-wing distributed propulsion refers to a propulsion system where multiple small engines, fans, or electric motors are embedded within the wing of an aircraft, typically distributed along the span.
This design aims to provide more efficient thrust generation and potentially improve overall aircraft performance by reducing drag and increasing lift.
The distributed nature of the propulsion system can also offer redundancy and improved safety, as the failure of one engine would not significantly impact the aircraft's ability to generate thrust.
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