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- W2243316701 abstract "In this paper the effects of fuselage bending on the longitudinal and lateral stability and dynamic flying characteristics of the aircraft is reviewed and the results of fuselage elasticity are studied using structural flexibility data and aerodynamic stability coefficients of a turboprop passenger aircraft. It is shown that fuselage bending can lead to a significant reduction in the longitudinal and lateral stability of the aircraft. The theoretical development of the nonlinear equations of motion considering the structural elasticity is reviewed and flight dynamics of the aircraft is simulated. In order to clearly demonstrate the elasticity effects, the dynamic simulation of the aircraft is carried out considering the aircraft with the exaggerated flexible fuselage. This simulation proves that the dynamic longitudinal and lateral responses of the aircraft are highly influenced by the fuselage bending caused by the horizontal and vertical tail forces." @default.
- W2243316701 created "2016-06-24" @default.
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- W2243316701 date "2009-01-01" @default.
- W2243316701 modified "2023-09-23" @default.
- W2243316701 title "Studying the effect of fuselage bending on flight dynamics and stability coefficients of a 50-seat turboprop passenger aircraft" @default.
- W2243316701 hasPublicationYear "2009" @default.
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