Keyphrases
Three-dimensional (3D)
83%
Planetary Gearbox
74%
Geared Rotor System
66%
State-space Model
58%
Gearbox
56%
Dynamic Behavior
42%
Rotating System
42%
Rotor
42%
Dynamic Model
41%
Experimental Identification
41%
Nonlinear Vibration
41%
Dynamic Analysis
38%
Gear Parameters
38%
Planet Gear
38%
Composite Wind Turbine Blade
33%
Gear Train
33%
Fuel Injection Pump
33%
Straight Beam
33%
Diesel Engine
33%
Impact Noise
33%
Joint Structure
33%
Model Identification
33%
Mode Model
33%
Polynomial Nonlinear State-space Model
33%
Space Mode
33%
Resonant Vibration
33%
Variable Angle Tow
33%
Aircraft Wing
33%
Flutter Characteristics
33%
Eigenvalue Solution
33%
Nonlinear Modal Testing
33%
Generalized Eigenvalue Problem
33%
Aeroelastic Tailoring
33%
Combat Aircraft
33%
Rotor System
33%
Whirl Flutter
33%
System Identification
33%
Standard Eigenvalues
33%
Modal Sensitivity
33%
Gyroscopic Effect
29%
Vibration Mode
24%
Mode Shape
21%
Finite Element Method
21%
Finite Element Model
21%
Modal Analysis
21%
Natural Frequency
17%
Six Degrees of Freedom
17%
Reinforced
16%
Maximum Deviation
16%
Varying Cross-section
16%
Engineering
Rotor System
100%
Gearbox
100%
Rotors
61%
Dynamic Behavior
39%
Numerical Study
37%
Combat Aircraft
33%
Aeroelastic Tailoring
33%
Sinusoidal Excitation
33%
Analytical Study
33%
Negative Damping
33%
Cross Section
33%
Diesel Engine
33%
Fuel Injection
33%
Impact Noise
33%
Nonlinear Term
33%
Gear Train
33%
Frictional Dissipation
33%
Periodic Motion
33%
Wings
33%
Bolted Joints
33%
Eigenvalue
33%
Damping Ratio ζ
33%
Priori Knowledge
33%
Compressed Air Motors
33%
Forced Vibration
33%
Vibration Mode
33%
Mode Shape
32%
Gyroscopic Effect
26%
Dynamic Models
26%
Transients
23%
Test Rig
23%
Resonant Frequency
22%
Core Material
22%
Axial Modes
22%
Gear Mesh
22%
Structural Constraint
22%
Lateral Vibration
22%
Finite Element Modeling
19%
Modal Analysis
19%
Natural Mode
18%
Finite Element Analysis
18%
Lap Joint
16%
Phase Locked Loop
16%
Cantilever Beam
16%
Basis Function
16%
Dynamic Range
16%
Polynomial Basis Function
16%
Nonlinear System Identification
16%
Predictive Capability
16%
Nonlinearity
16%
