Application of modern polymeric composite materials in the design of MS-21 airplane family

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This work contains an overview of the general implementation issues of polymeric composites in airframe structure of MS-21 airplane family. Here is a review of tasks and the current results of developmental works on composite units - wing and tail.

Composite, carbon, wing, tail, developmental work

Короткий адрес: https://sciup.org/148201260

IDR: 148201260

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