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A dynamic rotating blade model at an arbitrary stagger angle based on classical plate theory and the Hamilton's principle

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TLDR
In this paper, a dynamic model based on classical plate theory is presented to investigate the vibration behavior of a rotating blade at an arbitrary stagger angle and rotation speed, and the Hamilton's principle is applied to the model.
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This article is published in Journal of Sound and Vibration.The article was published on 2013-03-04. It has received 58 citations till now. The article focuses on the topics: Hamilton's principle & Plate theory.

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Citations
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General shell model for a rotating pretwisted blade

TL;DR: In this article, a novel dynamic model for a pretwisted rotating compressor blade mounted at an arbitrary stagger angle using general shell theory and including the rotational velocity is developed to study the eigenfrequencies and damping properties of the pre-strained rotating blade.
Journal ArticleDOI

Free vibration analysis of a pre-twisted sandwich blade with thermal barrier coatings layers

TL;DR: In this paper, a rotating cantilever sandwich-plate model with a pre-twisted and pre-set angle has been developed to investigate the vibrational behavior of an aero-engine turbine blade with thermal barrier coating (TBC) layers.
Journal ArticleDOI

Nonlinear dynamic responses of rotating pretwisted cylindrical shells

TL;DR: In this paper, a rotating pretwisted cylindrical shell model with a presetting angle is established to investigate nonlinear dynamic responses of the aero-engine compressor blade.
Journal ArticleDOI

Vibration characteristics of a rotating pre-twisted composite laminated blade

TL;DR: In this article, a new dynamic model based on the shell theory is presented to investigate the vibration behavior of a rotating composite laminated blade with a pre-twisted angle, where the effects of the Coriolis and centrifugal forces due to the rotation motion of the blade are considered in the formulation.
Journal ArticleDOI

Free vibration of rotating cantilever pre-twisted panel with initial exponential function type geometric imperfection

TL;DR: In this paper, a new vibration model for the rotating blade which is treated as a cantilever pre-twisted panel with initial exponential function type geometric imperfection is provided by using the shallow shell theory in which the torsion is considered but the two radii of curvatures are zero.
References
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Journal ArticleDOI

Free Vibration Analysis of Rotating Cantilever Plates

TL;DR: Linearized equations of motion for the free vibration analysis of rotating cantilever plates are derived in this article, where two inplane stretch variables are introduced and approximated to obtain the ordinary differential equation of motion.
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Free vibration of a rotating non-uniform beam with arbitrary pretwist, an elastically restrained root and a tip mass

TL;DR: In this article, the Hamilton's principle was used to derive the governing differential equations for the coupled bending-bending vibration of a rotating beam with a tip mass, arbitrary pretwist, an elastically restrained root, and rotating at a constant angular velocity.
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Dynamics of advanced rotating blades made of functionally graded materials and operating in a high-temperature field

TL;DR: In this paper, the effects of the extension-twist elastic coupling in conjunction with the volume fraction of the two constituent phases and of the thermal degradation of material properties on eigenfrequencies are discussed.
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Equations of motion of a blade rotating with variable angular velocity

TL;DR: In this article, the equations of motion of a blade mounted on a disk rotating with variable angular velocity are derived and the acceleration of the disk is taken as constant and the calculus of variations is employed to obtain the equation governing the ensuing free vibrations.
Journal ArticleDOI

Free vibrations of rotating small aspect ratio pretwisted blades

TL;DR: In this paper, the free vibration characteristics of a rotating pretwisted small aspect ratio blade, mounted on a disc at a stagger angle, are determined using classical bending theory of thin shells.
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