Keyphrases
Evolutionary Method
100%
Airfoil
100%
Elastic Panel
100%
Tonal Noise Reduction
100%
Airfoil Noise
100%
Noise Reduction
88%
Panel Design
44%
Boundary Layer Instability
44%
Trailing Edge
33%
Flow-induced Vibration
22%
Direct Aeroacoustic Simulation
22%
Flow Fluctuation
22%
Aeroacoustic Feedback Loop
22%
Nonlinear Equations
11%
Computation Time
11%
Reynolds number
11%
Element Method
11%
Dynamic Equations
11%
Continuous Flow
11%
Directivity
11%
Resource Requirements
11%
Feasible Method
11%
High-frequency Noise
11%
Dominant Frequency
11%
Design Yield
11%
Nonlinear Interaction
11%
Computational Resources
11%
Strong Reduction
11%
Flow Effect
11%
Low Computational
11%
Best Location
11%
Mach number
11%
Stationary Solution
11%
Gaussian Pulse
11%
Tonal Noise
11%
Non-resonant
11%
Optimal Noise
11%
Broadband Excitation
11%
Angle of Attack
11%
Separation Bubble
11%
Discrete Gaussian
11%
Noise Radiation
11%
Boundary Layer Flow
11%
Suction Surface
11%
Baseflow
11%
Panel Vibration
11%
Airfoil Flow
11%
Coupling Scheme
11%
Natural Boundary
11%
Tonal Reduction
11%
Design Iteration
11%
Fluid Load
11%
Monolithic Coupling
11%
Loaded Natural Frequency
11%
Low Noise
11%
NACA 0012
11%
Standard Finite Difference Method
11%
Engineering
Airfoil
100%
Boundary Layer
30%
Trailing Edge
23%
Structural Parameter
15%
Structural Panels
15%
Flow Fluctuation
15%
Feedback Loop
15%
Flow-Induced Vibrations
15%
Computational Resource
7%
Azimuthal
7%
Reynolds' Number
7%
Computational Time
7%
Element Method
7%
Suction Surface
7%
Feasibility Study
7%
Angle-of-Attack
7%
Separation Bubble
7%
Gaussians
7%
Design Iteration
7%
Natural Boundary
7%
Mach Number
7%
Directivity
7%
Resonant Frequency
7%
Finite Difference Method
7%
Base Flow
7%