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- W1523144179 abstract "The paper presents numerical analysis of airplane parameters of motion during wing transverse vibrations of an average commercial airplane. The mathematical model of the airplane motion including a system of twelve ordinary differential equations was employed. Using available publications and M28 Bryza airplane geometrical and mass relationships, a computer code evaluating parameters of the motion was developed. In order to take the wing transverse vibrations under consideration, the way of wing displacements in the aircraft-fixed system of coordinates was elaborated as well as vibration amplitude and frequency were assumed. The analysis covered two cases of wing transverse vibrations: bending of both wing halves in phase and in counter-phase. On the basis of the obtained results, some conclusions referring the airplane dynamic properties during wing vibrations were formulated." @default.
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- W1523144179 date "2010-01-01" @default.
- W1523144179 modified "2023-09-26" @default.
- W1523144179 title "The influence of wing transverse vibrations on dynamic parameters of an aircraft" @default.
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