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Effects of a cracked blade on mistuned turbine engine rotor vibration
Akira Saito
, Matthew P. Castanier
,
Christophe Pierre
Department of Mechanical Engineering
Stevens Institute of Technology
Research output
:
Contribution to journal
›
Article
›
peer-review
Overview
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Dive into the research topics of 'Effects of a cracked blade on mistuned turbine engine rotor vibration'. Together they form a unique fingerprint.
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Keyphrases
Mistuning
100%
Rotor Vibration
100%
Cracked Blade
100%
System Response
40%
Reduced Order Model
40%
Forced Response
40%
Hybrid Interface
40%
Component Mode Synthesis
40%
Computational Efficiency
20%
Multiple Families
20%
Rotational Speed
20%
Interface Method
20%
Response Prediction
20%
Three-dimensional Space
20%
Degrees of Freedom
20%
Nonlinear Equations
20%
Finite Element Model
20%
Reduced Order Modeling
20%
Time Integration
20%
Resonance Frequency Shift
20%
Forced Vibration Response
20%
Rotor
20%
Interface Components
20%
Time-domain Method
20%
Families of Systems
20%
Vibration Characteristics
20%
Stiffness Loss
20%
Steady Motion
20%
Crack Surface
20%
Time-frequency Domain
20%
System Vibration
20%
System Mode
20%
Vibration Localization
20%
Nonlinear Forced Vibration
20%
Alternating Frequency
20%
Engineering
Rotors
100%
Reduced Order Model
66%
System Response
66%
Force Response
66%
Synthesis Method
33%
Finite Element Modeling
33%
Degree of Freedom
33%
Frequency Shift
33%
Dimensional Space
33%
Simple Model
33%
Characteristic Vibration
33%
Time Domain Processing
33%
Rotation Speed
33%
Crack Surface
33%
System Mode
33%
Forced Vibration
33%
Resonant Frequency
33%
Rigidity
33%
Nonlinear Equation
33%