Keyphrases
Aircraft Wing
37%
Approximate Solution
30%
Beam Model
29%
Cantilever
23%
Cantilever Beam
20%
Composite Timoshenko Beam
25%
Computer Package
23%
Differential Equations of Motion
58%
Differential Transform Method
96%
Double-tapered
34%
Elastic Soil
22%
Equations of Motion
73%
Euler-Bernoulli Beam
43%
Flapwise
23%
Flapwise Bending Vibration
70%
Flutter Analysis
28%
Free Vibration Analysis
77%
Governing Differential Equation
41%
Hamilton's Principle
28%
He's Variational Method
21%
Helicopter Blade
25%
High-order
25%
Hub Radius
51%
Incompressible Flow
25%
Kinetic Energy
24%
Limit Cycle Oscillation
25%
Mathematica
25%
Mathematical Techniques
23%
Mode Shape
25%
Natural Frequency
81%
Nonlinear Oscillator
51%
Nonlinear Transverse Vibration
25%
Numerical Results
20%
Parameter Expansion
24%
Ply Angle
21%
Ply Orientation
23%
Potential Energy
29%
Rotary Inertia
23%
Rotating Timoshenko Beam
25%
Rotational Speed
38%
Shear Deformation
28%
Slenderness Ratio
38%
Strip Theory
23%
Sweep Angle
25%
Swept-back Wing
20%
Taper Ratio
27%
Thin-walled Composite Beams
84%
Transverse Shear
29%
Twist-stretch Coupling
20%
Vibration Analysis
89%
Engineering
Accurate Solution
25%
Active Vibration Control
17%
Aerodynamic Load
20%
Amplitude-Frequency Relation
19%
Approximate Solution
30%
Approximation Order
38%
Beam Model
34%
Bending Vibration
77%
Bernoulli Beam
47%
Boundary Condition
20%
Cantilever Beam
20%
Cross Section
22%
Dynamic Stability
25%
Feedback Control System
15%
Finite Element Method
36%
Flutter Speed
15%
Free Vibration
15%
Free Vibration Analysis
82%
Genetic Algorithm
17%
Good Agreement
44%
Governing Differential Equation
50%
Hamilton's Principle
38%
Hamiltonian
17%
Helicopter Blade
25%
Illustrates
32%
Incompressible Flow
27%
Leading Edge
18%
Limit Cycle
25%
Mathematical Model
17%
Mathematical Technique
30%
Mode Shape
27%
Natural Frequency
100%
Piezoelectric
15%
Ply Angle
23%
Ply Orientation
24%
Potential Energy
34%
Relative Error
21%
Rotary Inertia
30%
Rotational Speed
53%
Rotor Blade
18%
Shear Deformation
52%
Simulation Method
23%
Slenderness Ratio
43%
Strip Theory
23%
Sweep Angle
26%
Thin-Walled Composite Beam
86%
Unmanned Aerial Vehicle
17%
Vibration Analysis
99%
Vortex
24%
Wings
43%