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Annotation
В данной работе производится расчет и проектирование основных элементов двухконтурного турбореактивного двигателя, мощностью 75 кН, предназначенного для региональных пассажирских перевозок.
In this work, the calculation and design of the main by-pass turbojet engine elements with a 75 kN thrust, intended for regional passenger traffic, is carried out.
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