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The problem of calculating the natural frequencies of a rotating bladed disk is solved by the Ritz method.
Numerical results indicate that the blade crack may be one of the reasons for the occurrence of the localization phenomenon in the rotating bladed disk.
In an attempt towards the understanding of coupling effects between shaft-torsional and blade-(in plane) bending vibrations in turbomachinery and other rotating bladed structures, an idealized model is considered where the blades are represented by uniform Euler Bernouilli beams.
The effects of blade crack on mode localization in rotating bladed disks are investigated in this study.
In turbomachinery applications, rotating bladed disks (blisks) are often subject to high levels of dynamic loading, such as traveling wave excitations, which result in large response amplitudes at resonance.
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The influence of changes in rotational speed on the dynamics of rotating blades is investigated.
Two finite element approaches are implemented to account for the rotational non-linearities involved in dynamic analysis of rotating bladed-disk assemblies: the distributed mass (DM) and lumped mass (LM) approaches.
Moreover, the increment of rotational speed will reduce the mean-square response of a rotating blade.
Minimizing the operating clearance between rotating bladed-disks and stationary surrounding casings is a primary concern in the design of modern turbomachines since it may advantageously affect their energy efficiency.
A water jet directed at rotating blade cools it and washes away tile debris.
How do marine animals interact with tidal turbines, which feature rotating blades that could kill them?
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com