Engineering
Vortex
71%
Synthetic Jet Actuator
56%
Circular Cylinder
54%
Reynolds' Number
50%
Energy Engineering
44%
Lattice-Boltzmann Method
38%
Vortex Induced Vibration
35%
Natural Convection
34%
Energy Harvesting
32%
Particle Image Velocimetry
27%
Rayleigh Number
26%
Phase Difference
26%
Orifice
24%
Vortex Shedding
24%
Flow Separation
24%
Aerodynamic Performance
23%
Two Dimensional
23%
Flow Distribution
22%
Parametric Study
22%
Computational Fluid Dynamics
21%
Actuation
20%
Airfoil
20%
Entropy Generation
20%
Facing Step
20%
Reinforcement Learning
20%
Fluid-Structure Interaction
19%
Turbulent Boundary Layer
19%
Active Control
17%
Flow Structure
16%
Laminar Boundary Layer
16%
Boltzmann Equation
16%
Unmanned Aerial Vehicle
16%
Aspect Ratio
16%
Helmholtz's Law
16%
Shear Layer
16%
Simulation Result
15%
Proper Orthogonal Decomposition
15%
Computer Simulation
14%
Leading Edge
14%
Turbulent Flow
14%
Eckert Number
13%
Separation Control
13%
Oscillatory
13%
Fluid Mechanics
13%
Boundary Condition
13%
Flow-Induced Vibrations
13%
Angle-of-Attack
13%
Harvester
12%
Fixed Wings
12%
Energy Flow
12%
Keyphrases
Synthetic Jet
100%
Synthetic Jet Actuator
54%
Reynolds number
47%
Circular Cylinder
39%
Vortex-induced Vibration
34%
Phase Difference
30%
Active Flow Control
29%
Flow Control
28%
Wing Model
25%
Entropy Generation
24%
Fluid-structure Interaction
24%
Heat Transfer
24%
Vortex
23%
Heave
23%
Actuator
23%
Aerodynamic Performance
22%
Deep Reinforcement Learning (deep RL)
21%
Viscoplastic Fluid
20%
Lattice Boltzmann Model
20%
Natural Convection
20%
Rayleigh number
20%
Lattice Boltzmann Method
19%
Actuation
19%
Turbulent Boundary Layers
18%
Airfoil
18%
Energy Harvesting
18%
Vortex Shedding
17%
Vortex Structure
17%
Machine Learning
17%
Active Control
17%
Heat Mass Transfer
16%
Time-resolved Particle Image Velocimetry (TR-PIV)
16%
Flow Field
16%
Blowing
16%
Helmholtz Resonance
15%
Heat Transfer Enhancement
15%
Laminar Boundary Layer
15%
Flow Structure
15%
Fluid Mechanics
15%
Particle Image Velocimetry Technique
14%
Orifice
14%
Aspect Ratio
13%
Jet Flow
13%
Flow-induced Vibration
13%
PIV Measurement
13%
In Tandem
13%
Hairpin Vortex
13%
Flap
12%
Proper Orthogonal Decomposition
12%
Tandem Configuration
12%
