We herein propose an algorithm for tracking smooth bifurcations of nonlinear systems with
interdependent parameters. The approach is based on a complex formulation of the well …

In this study, a computational fluid dynamics (CFD) based reduced-order modeling (ROM)
approach robust to flight parameter variations is presented. The approach, which uses …

The paper describes a free-flutter experiment on a stand-alone low-pressure turbine bladed
rotor in a high-speed rotating wind tunnel together with the most relevant design decisions …

In turbomachinery, understanding the interaction between blade vibrations and the tip flow is
of great interest due to current trends, which tend to thinner airfoils with higher loading and …

Bifurcations organize the dynamics of many natural and engineered systems. They induce
qualitative and quantitative changes to a system's dynamics, which can have catastrophic …

In this study, an improved nonlinear reduced-order model composed of a linear part and a
nonlinear part is explored for transonic aeroelastic systems. The linear part is identified via …

Axial flow turbomachinery is susceptible to self-excited vibrations known as flutter, primarily
affecting high-aspect ratio rotor blades. Experimental studies of blade flutter are essential to …

Accurate and efficient predictions of the steady and unsteady flow responses due to the
blade-to-blade variation as well as due to the nonaxisymmetric inlet distortion have been …

Blade flutter of modern gas-turbine engines is one of the main issues that engine designers
have to face. The most used numerical method that is employed for flutter prediction is the …

Assembly interface of aircraft vertical tail is a large thin-wall structure and made from titanium
alloys, which causes easily machining vibration, deformation and undercutting in finish …