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- Article name
- Rational design of composite fuselage compartment structure
- Authors
- DUDCHENKO A. A., , a_dudchenko@mail.ru, Moscow Aviation Institute (National Research University), Moscow, Russia
R. A. CANCHAYA ROJAS , , raul_angel@mail.ru, Moscow Aviation Institute (State Technical University), Moscow, Russia
- Keywords
- rational design / composite materials / constructive and power schema of fuselage / frame / stringer / fuselage compartment
- Year
- 2011 Issue 2 Pages 21 - 34
- Code EDN
- Code DOI
- Abstract
- The article presents a rational design method of composite fuselage compartment structure, providing reliable work of a structure at a minimum of weight and at restrictions on durability, rigidity and stability taking into account is constructive-technological restrictions. The spent estimation of accuracy of the results received with use of the offered method with results received by finite element method (FEM) has shown that this method provides necessary accuracy of calculations.
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