Wing stiffness, mainly including bending stiffness and torsion stiffness, is very important in aircraft structure design. In order to research the relation between wing stiffness and optimization results, this paper makes optimization analysis to a composite T-tail configuration and a composite flying wing configuration based on different wing stiffness constraints, and some valuable conclusions are achieved.
Structural Optimization Research of Composite Aircraft Based on Different Wing Stiffness Constraints
Advanced Materials Research ; 466-467 ; 282-286
2012-02-10
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2016
|