Research on flutter method for three dimensional wing rudder
Xiaoyi Zhou, Liang Li, Lan Yang, Jun Xiao, Qing-Chun Zhang
Abstract
Open-access reader
Xiaoyi Zhou, Liang Li, Lan Yang, Jun Xiao, Qing-Chun Zhang
Abstract
Open-access reader
Abstract Aiming at providing high efficiency and accurate flutter analysis for high speed aircraft in transonic flow, flutter analysis in frequency domain based on three-dimensional wing rudder is employed for AGARD 445.6 wing. The simulation results are consistent with both experiment and reference, which validates the flutter mechanism in the subsonic and transonic regions. This simulation not only improves the accuracy of flutter analysis, but also saves calculation time and improves efficiency. Thus, it lays a foundation for high speed aircraft in transonic flow flutter prediction.
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Abstract Aiming at providing high efficiency and accurate flutter analysis for high speed aircraft in transonic flow, flutter analysis in frequency domain based on three-dimensional wing rudder is employed for AGARD 445.6 wing. The simulation results are consistent with both experiment and reference, which validates the flutter mechanism in the subsonic and transonic regions. This simulation not only improves the accuracy of flutter analysis, but also saves calculation time and improves efficiency. Thus, it lays a foundation for high speed aircraft in transonic flow flutter prediction.
Key concepts: Flutter, Transonic, Rudder, Wing, Airfoil, Aeroelasticity, Aerospace engineering, Computer science