[HTML][HTML] Application of immersed boundary method in turbomachines

C Congcong, W Yuwei, W Zhuo, DU Lin… - Chinese Journal of …, 2023 - Elsevier
Simulating unsteady turbulent flow in turbomachines is still challenging due to the
complexity of blade geometry and relative motion between rotor and stator. This study …

The effect of aerodynamic asymmetries on turbomachinery flutter

K Ekici, RE Kielb, KC Hall - Journal of Fluids and Structures, 2013 - Elsevier
In this paper, the effect of aerodynamic asymmetries on the flutter characteristics of
turbomachinery blades is investigated. Specifically, the present method is used to study the …

Nonlinear Dynamics of the High‐Speed Rotating Plate

M Yao, L Ma, W Zhang - International Journal of Aerospace …, 2018 - Wiley Online Library
High speed rotating blades are crucial components of modern large aircraft engines. The
rotating blades under working condition frequently suffer from the aerodynamic, elastic and …

Natural frequency clusters in planetary gear vibration

TM Ericson, RG Parker - … of Vibration and …, 2013 - asmedigitalcollection.asme.org
This paper investigates how the natural frequencies of planetary gears tend to gather into
clusters (or groups). This behavior is observed experimentally and analyzed in further detail …

Optimization of nonlinear hyperelastic coefficients for foot tissues using a magnetic resonance imaging deformation experiment

M Petre, A Erdemir… - Journal of …, 2013 - asmedigitalcollection.asme.org
Accurate prediction of plantar shear stress and internal stress in the soft tissue layers of the
foot using finite element models would provide valuable insight into the mechanical etiology …

Eddy current-based vibration suppression for finish machining of assembly interfaces of large aircraft vertical tail

W Fan, L Zheng, W Ji, X Zhao… - Journal of …, 2019 - asmedigitalcollection.asme.org
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 …

Effects of nonuniform blade spacing on compressor rotor forced response and aeroacoustics

Y Leng, NL Key - Journal of Propulsion and Power, 2020 - arc.aiaa.org
A generalized flat plate cascade model is developed in this study to predict the unsteady
aerodynamics of a blade row with circumferentially nonuniform spacing in subsonic …

The effects of aerodynamic asymmetric perturbations on forced response of bladed disks

T Miyakozawa, RE Kielb, KC Hall - 2009 - asmedigitalcollection.asme.org
Most of the existing mistuning research assumes that the aerodynamic forces on each of the
blades are identical except for an interblade phase angle shift. In reality, blades also …

Effects of downstream vane bowing and asymmetry on unsteadiness in a transonic turbine

JP Clark, RJ Anthony, MK Ooten… - Journal of …, 2018 - asmedigitalcollection.asme.org
Accurate predictions of unsteady forcing on turbine blades are essential for the avoidance of
high-cycle-fatigue issues during turbine engine development. Further, if one can …

[图书][B] Flutter and forced response of turbomachinery with frequency mistuning and aerodynamic asymmetry

T Miyakozawa - 2008 - search.proquest.com
This dissertation provides numerical studies to improve bladed disk assembly design for
preventing blade high cycle fatigue failures. The analyses are divided into two major …