Keyphrases
Aeroacoustics
100%
Flow Field
64%
Numerical Results
40%
Cantilever Probe
34%
Wafer Probe
34%
Cavity Flow
31%
Turbulence Model
31%
Numerical Investigation
27%
Hydroacoustics
27%
Generative Adversarial Networks
27%
Airfoil
27%
Numerical Solution
20%
Temperature Distribution
20%
Current Carrying Capacity
20%
Detached Eddy Simulation
20%
Source Code
20%
Computational Fluid Dynamics
20%
Laminar Airflow
20%
Computational Fluid Dynamics Software
18%
Low Mach number Flow
17%
Hydrofoil
16%
Process Optimization
16%
Unsteady Flow Field
16%
Sound Generation
13%
Open Cavity
13%
Modified Geometry
13%
Mesh number
13%
On-wafer Measurement
13%
Thickness Noise
13%
Helicopter Rotor Noise
13%
Experimental Characterization
13%
Joule Heating
13%
Unsteady Flow
13%
Non-reflecting Boundary Condition
13%
Wafer
13%
Test Probe
13%
Special Design
13%
Maximum Current
13%
Headwind
13%
Backward-facing Step
13%
Dynamic Source
13%
Weapons Bay
13%
Transonic Flow
13%
Control Configuration
13%
Large Eddy Simulation
13%
Transient Heat Transfer
13%
Airflow
13%
Predictive Models
13%
Blockage Effect
13%
Flow Behavior
13%
Engineering
Flow Distribution
64%
Computational Fluid Dynamics
41%
Experimental Result
34%
Cavity Flow
31%
Temperature Distribution
27%
Air Flow
27%
Airfoil
27%
Unsteady Flow
25%
Low Mach Number
25%
Sound Pressure Level
23%
Numerical Solution
20%
Resistance Heating
20%
Detached Eddy Simulation
19%
Drag Coefficient
18%
Good Agreement
18%
Hydrofoil
18%
Angle-of-Attack
18%
Open Cavity
13%
Configuration Control
13%
Test Probe
13%
Probe Tip
13%
Blockage Effect
13%
Flow Behavior
13%
Transonic Flow
13%
Cavity Length
13%
Cavitation Number
13%
Experimental Characterization
13%
Facing Step
13%
Helicopter Rotors
13%
Current Carrying Capacity
13%
Dissipation Rate
13%
Heat Losses
13%
Crosswind
13%
Sound Generation
13%
Leading Edge
13%
Boundary Condition
13%
Aerodynamic Analysis
13%
Optimal Geometry
11%
Learning System
11%
Transients
11%
Blade Profile
11%
Experimental Measurement
9%
Discretization
9%
Front Wall
9%
Thickness Noise
9%
Blade Tip
9%
Field Result
8%
Finite Volume Method
8%
Mach Number
8%
Velocity Vector
6%
