Stability of Very Flexible Aircraft with Coupled Nonlinear Aeroelasticity and Flight Dynamics
Stability of Very Flexible Aircraft with Coupled Nonlinear Aeroelasticity and Flight Dynamics
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DOI：
10.2514/1.c034162
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发表时间：
2017-10
影响因子：
2.2
通讯作者：
Changchuan Xie;Yang Lan;Liu Yi;Yang Chao
中科院分区：
文献类型：
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作者：
Changchuan Xie;Yang Lan;Liu Yi;Yang Chao
本文提出了一个框架，用于分析一个非常灵活的飞机的稳定性特性，同时考虑到非线性气动弹性和飞行动力学。在这里，d...
This paper presents a framework for analyzing the stability characteristics of a very flexible aircraft, simultaneously taking into account nonlinear aeroelasticity and flight dynamics. Here, the d...