A review of computational methods and reduced order models for flutter prediction in turbomachinery

M Casoni, E Benini - Aerospace, 2021 - mdpi.com
Aeroelastic phenomena in turbomachinery are one of the most challenging problems to
model using computational fluid dynamics (CFD) due to their inherent nonlinear nature, the …

Exact H2 Optimal Tuning and Experimental Verification of Energy-Harvesting Series Electromagnetic Tuned-Mass Dampers

Y Liu, CC Lin, J Parker, L Zuo - … of Vibration and …, 2016 - asmedigitalcollection.asme.org
Energy-harvesting series electromagnetic-tuned mass dampers (EMTMDs) have been
recently proposed for dual-functional energy harvesting and robust vibration control by …

Mistuned forced response predictions of an embedded rotor in a multistage compressor

FM Besem, RE Kielb, P Galpin… - Journal of …, 2016 - asmedigitalcollection.asme.org
This paper covers a comprehensive forced response analysis conducted on a multistage
compressor and compared with the largest forced response experimental data set ever …

Aeroelastic analysis of a varying thickness blade with temperature-dependent sandwich materials by using isogeometric method

S Zhong, G Jin, Q Gong, Y Chen, N Wang - Thin-Walled Structures, 2024 - Elsevier
Aeroelastic stability is a common vibration problem for rotating machinery. In this paper, the
aeroelastic stability problem of the blade is treated as a matrix eigenvalue solution, in which …

Review of Vibration Analysis and Structural Optimization Research for Rotating Blades

S Zhong, G Jin, Y Chen, T Ye, T Zhou - Journal of Marine Science and …, 2024 - Springer
Blades are important parts of rotating machinery such as marine gas turbines and wind
turbines, which are exposed to harsh environments during mechanical operations, including …

Influence of the tip clearance on a compressor blade aerodynamic damping

FM Besem, RE Kielb - Journal of Propulsion and Power, 2017 - arc.aiaa.org
The flutter CFD calculations conducted in industry generally use a single-row, single-
passage approach with a minimum of detailing to reduce the computational time as much as …

Forced response sensitivity of a mistuned rotor from an embedded compressor stage

FM Besem, RE Kielb, NL Key - Journal of …, 2016 - asmedigitalcollection.asme.org
The frequency mistuning that occurs due to manufacturing variations and wear and tear of
the blades has been shown to significantly affect the flutter and forced response behavior of …

A reduced order model for uncoupled and coupled cascade flutter analysis

D Su, W Zhang, Z Ye - Journal of Fluids and Structures, 2016 - Elsevier
It is computation-intensive and time-consuming to conduct the direct numerical simulation of
the fluid and structure interaction of an entire blade row. This paper presents a reduced …

Forced response sensitivity of a mistuned rotor from an embedded compressor stage

FM Besem, RE Kielb, NL Key - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
The frequency mistuning that occurs due to manufacturing variations and wear and tear of
the blades can have a significant effect on the flutter and forced response behavior of a …

Multi-Passage harmonic balance method for flutter prediction in multi-row configurations

D Zhou, Z Ji, J Wu, E Shen, T Guo, Z Lu - Aerospace Science and …, 2024 - Elsevier
A multi-passage harmonic balance method is presented for flutter prediction in multi-row
configurations, and particular focus is on simulation of more than two blade rows. The …