The Stability of Longitudinal Motion of Amphibious Aircraft During Takeoff

In this paper, the mathematical model of the takeoff of an amphibious aircraft was established. On this basis, the hydrodynamic coefficients in the pitch and heave motion equation were calculated using the strip theory. The stability criterion was used to analyze the longitudinal motion stability of...

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Veröffentlicht in:Journal of physics. Conference series 2023-08, Vol.2569 (1), p.12070
Hauptverfasser: Shi, Sheng-zhe, Gao, Xian-Jiao, Jiang, Ting, Sang, Teng-jiao
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Jiang, Ting
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description In this paper, the mathematical model of the takeoff of an amphibious aircraft was established. On this basis, the hydrodynamic coefficients in the pitch and heave motion equation were calculated using the strip theory. The stability criterion was used to analyze the longitudinal motion stability of the amphibious aircraft during takeoff, and three characteristic parameters of the general stability of longitudinal motion were obtained: natural period, half-decay period, and damping ratio. The result showed that the motion of amphibious aircraft was stable during takeoff.
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subjects Aircraft stability
Amphibious aircraft
Damping ratio
Equations of motion
Hydrodynamic coefficients
Motion stability
Physics
Stability analysis
Stability criteria
Takeoff
title The Stability of Longitudinal Motion of Amphibious Aircraft During Takeoff
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