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Finite element modeling of compressor blade leading edge curl, erosion and deformation
George M. Slota
,
Douglas E. Wolfe
Office of the Senior Vice President for Research
Engineering Science and Mechanics
Ken and Mary Alice Lindquist Department of Nuclear Engineering
Materials Science and Engineering
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Dive into the research topics of 'Finite element modeling of compressor blade leading edge curl, erosion and deformation'. Together they form a unique fingerprint.
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Keyphrases
Compressor Blade
100%
Finite Element Modeling
100%
Blade Leading Edge
100%
Blade Deformation
100%
Particle Size
50%
Two Dimensional
50%
Three-dimensional (3D)
50%
Impact Angle
50%
Finite Element Method
50%
Large Particle
50%
Deformation Measurement
50%
Component-based
50%
Engine Performance
50%
Particle Impact
50%
Sandy Environment
50%
Impingement Angle
50%
Blade Model
50%
Shape Deformation
50%
Aerodynamic Properties
50%
Simulation Parameters
50%
Preventive Methods
50%
Dusty Environment
50%
Engineering
Leading Edge
100%
Compressor Blades
100%
Fem Model
100%
Particle Diameter
20%
Impact Angle
20%
Engine Performance
20%
Blade Model
20%
Finite Element Analysis
20%
Turbine
20%
Aerodynamic Property
20%
Simulation Parameter
20%
Material Science
Aircraft
100%
Finite Element Modeling
100%
Finite Element Method
50%