Engineering
Energy Engineering
100%
Piezoelectric
60%
Harvester
59%
Nonlinearity
50%
Energy Harvesting
48%
Airfoil
37%
Load Resistance
29%
Aerodynamic Load
29%
Vortex
26%
Degree of Freedom
24%
Angle-of-Attack
22%
Limit Cycle
20%
Micro Air Vehicle
20%
Nonlinear Analysis
19%
Reduced Order Model
19%
Lattice Method
15%
Wave Energy
14%
Pressure Coefficient
14%
Electrical Load
14%
Multiple Scale
13%
Peak Pressure
13%
Frequency Component
13%
Circular Cylinder
13%
Cantilever Beam
13%
Flaps
12%
Ultrasonics
12%
Power Converter
12%
Pressure Fluctuation
11%
Frequency Response
11%
Computer Simulation
11%
Natural Frequency
11%
Vortex Induced Vibration
11%
Approximate Solution
11%
Hopf Bifurcation
10%
Spectral Moment
10%
Hydrodynamics
10%
Control Surfaces
10%
Mixing Layer
10%
Forward Flight
10%
Flight Dynamics
10%
Reynolds' Number
10%
Flutter Speed
10%
Lift Coefficient
10%
Non-Linear Dynamic
10%
Nonlinear Parameter
9%
Experimental Investigation
9%
Cross Section
9%
Wind Turbine
9%
Trailing Edge
8%
Transducer
7%
Keyphrases
Airfoil
33%
Harvested Power
32%
Hovering
29%
Energy Harvesting
28%
Flap
27%
Aeroelastic System
27%
Load Resistance
26%
Energy Harvester
26%
Piezoelectric Energy Harvester
24%
Aerodynamic Loads
24%
Piezoelectric Energy Harvesting
19%
Harvester
19%
Limit Cycle Oscillation
18%
Piezoaeroelastic
18%
Nonlinear Analysis
16%
Reduced Order Model
16%
Mean Flow
16%
Angle of Attack
15%
Galloping
15%
Turbulence
14%
Low-rise Building
14%
Pressure Coefficient
14%
Nonlinearity
14%
Degrees of Freedom
13%
Electrical Load
13%
Surface Mounting
13%
Flutter
13%
Multiscale Method
12%
Freeplay Nonlinearity
12%
Cantilever Beam
12%
Flapping-wing Micro Air Vehicle
12%
Governing Equation
11%
Control Surface
11%
Natural Frequency
11%
Circular Cylinder
11%
Kinematics
11%
Approximate Solution
11%
Unsteady Vortex Lattice Method
11%
Nonlinear Aeroelastic
11%
Flutter Speed
11%
Vortex-induced Vibration
10%
Bifurcation
10%
Load Coefficient
10%
Gust
10%
Free Play
10%
Aerodynamics
10%
Numerical Simulation
10%
Nonlinear Parameter
10%
Spectral Moments
10%
Forward Flight
10%
