Keyphrases
Differential Transform Method
97%
Vibration Analysis
89%
Thin-walled Composite Beams
85%
Natural Frequency
81%
Free Vibration Analysis
78%
Equations of Motion
73%
Flapwise Bending Vibration
71%
Differential Equations of Motion
58%
Nonlinear Oscillator
52%
Hub Radius
51%
Euler-Bernoulli Beam
43%
Governing Differential Equation
41%
Rotational Speed
38%
Slenderness Ratio
38%
Aircraft Wing
37%
Double-tapered
34%
Approximate Solution
30%
Potential Energy
29%
Transverse Shear
29%
Beam Model
29%
Flutter Analysis
28%
Shear Deformation
28%
Hamilton's Principle
28%
Taper Ratio
27%
Limit Cycle Oscillation
26%
High-order
26%
Composite Timoshenko Beam
26%
Rotating Timoshenko Beam
26%
Nonlinear Transverse Vibration
26%
Helicopter Blade
26%
Incompressible Flow
26%
Mode Shape
26%
Mathematica
26%
Sweep Angle
25%
Parameter Expansion
24%
Kinetic Energy
24%
Rotary Inertia
23%
Mathematical Techniques
23%
Cantilever
23%
Strip Theory
23%
Ply Orientation
23%
Computer Package
23%
Flapwise
23%
Elastic Soil
22%
He's Variational Method
21%
Ply Angle
21%
Numerical Results
20%
Swept-back Wing
20%
Cantilever Beam
20%
Twist-stretch Coupling
20%
Engineering
Resonant Frequency
100%
Vibration Analysis
99%
Thin-Walled Composite Beam
85%
Free Vibration Analysis
83%
Bending Vibration
78%
Oscillator
73%
Rotational Speed
53%
Aspect Ratio
52%
Shear Deformation
52%
Governing Differential Equation
50%
Bernoulli Beam
47%
Good Agreement
45%
Wings
43%
Finite Element Analysis
41%
Hamilton's Principle
39%
Potential Energy
34%
Beam Model
34%
Approximate Solution
30%
Mathematical Technique
30%
Rotary Inertia
30%
Incompressible Flow
27%
Mode Shape
27%
Sweep Angle
26%
Approximation Order
26%
Limit Cycle
26%
Helicopter Blade
26%
Dynamic Stability
26%
Ply Orientation
24%
Vortex
24%
Strip Theory
23%
Simulation Method
23%
Illustrates
22%
Cross Section
22%
Flaps
22%
Accurate Solution
21%
Amplitude-Frequency Relation
21%
Ply Angle
21%
Aerodynamic Load
21%
Cantilever Beam
20%
Boundary Condition
20%
Leading Edge
18%
Rotor Blade
18%
Feedback Control
18%
Relative Error
17%
Unmanned Aerial Vehicle
17%
Genetic Algorithm
17%
Mathematical Model
17%
Active Vibration Control
17%
Flight Condition
16%
Flutter Speed
15%