Analytical calculation of composite fuselage structure | Mekhanika | kompozitsionnykh | materialov i konstruktsii
> Volume 17 > №1 / 2011 / Pages: 133-144

Analytical calculation of composite fuselage structure

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Abstract:

In this work are developed analytical method and computer programs for to estimate the parameters of composite fuselage structure elements for the commercial transport aircraft. The present method, algorithms and computer programs allow to estimate the intense-deformed condition, durability and to optimize projects.

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