A wind tunnel experimental investigation of self-sustained oscillations of an aeroelastic
NACA0012 airfoil occurring in the transitional Re regime is presented. To the authors' …

The aeroelastic response of a NACA 0012 airfoil in the flow regimes prior to flutter is
investigated in a wind tunnel. We observe intermittent bursts of periodic oscillations in the …

The process of blending observational data in numerical models can be formulated using
the Bayesian estimation method. The Bayesian statistical framework strives to find the best …

MORPHING aircrafts may adapt themselves to multiple different missions given during their
flight by changing their morphological shape and mechanical characteristics [1]. This …

This paper proposes a generalized eigenvalue-based probability density evolution method
for aeroelastic systems considering stochastic uncertainties in structural and aerodynamic …

Methods for predicting the onset of flutter during an experiment are traditionally applied
treating the data as deterministic values. Uncertainty and variation in the data is often …

A Bayesian statistical framework is presented for Zimmerman and Weissenburger flutter
margin method which considers the uncertainties in aeroelastic modal parameters. The …

This paper presents an overview on flutter boundary prediction in tests which is principally
based on a system stability measure, named Jury's stability criterion, defined in the discrete …

发展了一种紊流激励条件下的颤振边界预测方法. 首先基于随机减量法从紊流激励响应中提取出
系统的自由衰减响应, 其次采用矩阵束法从自由衰减响应中识别出振动响应的主要模态参数 …

In flutter tests, particularly in wind tunnel experiments, the aircraft model is generally excited
by atmospheric turbulence, which increases the difficulty in precisely identifying the modal …