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Keyphrases
Airfoil
91%
Large Eddy Simulation
83%
De-icing
69%
Dielectric Properties
52%
Contrails
48%
Noise Prediction
47%
Polyethylene
46%
Near-field
45%
Microphysics
44%
Aircraft Engine
43%
Polystyrene
42%
Reynolds number
41%
Few-layer Graphene
39%
Graphene
38%
Ice Accretion
38%
Contrail Formation
38%
Heat Transfer
37%
Tip Gap
37%
Noise Source
36%
Broadband Noise
35%
Noise Generation Mechanism
33%
Soot
32%
Tip Leakage Vortex
32%
Direct numerical Simulation
30%
Rheological Properties
30%
Reynolds-averaged Navier-Stokes
29%
Surface Roughness
29%
Numerical Simulation
29%
Electrical Properties
29%
Tip Leakage Flow
28%
Installation Effects
28%
Gas Turbine Engine
27%
Preliminary Design Phase
26%
High-density Polyethylene
25%
Graphene Nanoplatelets
25%
Tip Noise
25%
Soot Particles
25%
Propeller
24%
Analytical Model
24%
Aircraft De-icing
24%
Icing
23%
Penalization
23%
Trailing Edge Noise
23%
Rotor
22%
Photodegradation
22%
Shear Layer
22%
Mach number
22%
High-pressure Turbine
22%
Serration
22%
Airport
22%
Computational Fluid Dynamics
21%
Operating Conditions
21%
Vortex
21%
Wall Pressure
21%
Polypropylene
21%
Ice Shedding
21%
Mechanical Properties
20%
Commercial Graphene
20%
Three-dimensional (3D)
20%
Clay
20%
Plume
19%
Rheological Behavior
19%
Nanoparticle Dispersion
19%
Rotor Blade
19%
Numerical Investigation
19%
Ice Accretion Simulation
18%
Ice Crystals
18%
Far-field Noise
18%
Fuel Sulfur Content
18%
Airfoil Noise
18%
Anti-icing
17%
Aeroderivative Gas Turbine
17%
Nanoparticles
17%
Butylenes
17%
Thermoplastic Elastomer
17%
Commercial Aircraft
16%
Aerosol Formation
16%
Maximum Lift Coefficient
16%
Turbulent Boundary Layers
16%
Adverse Pressure Gradient
16%
NARX Model
16%
Ducted Tail Rotor
16%
Molecular Dynamics
16%
Linear Low-density Polyethylene (LLDPE)
16%
Polyamide 1010
16%
Styrenic Block Copolymers
16%
Electrical Conductivity
16%
Wind Tunnel
16%
Flow Solver
16%
Eulerian
16%
Nanofillers
16%
Hexagonal Boron Nitride (h-BN)
16%
RANS Simulation
16%
Graphene Oxide
16%
Acoustics
16%
Flat Plate
16%
Microphysical Model
15%
Flow around
15%
Turbulence Model
15%
Aerofoil
15%
Engineering
Airfoil
100%
Aircraft
93%
Computational Fluid Dynamics
79%
Large Eddy Simulation
77%
Snow and Ice Removal
68%
Rotors
51%
Ice Accretion
49%
Jet
39%
Fan
37%
Noise Source
33%
Aircraft Engine
30%
Reynolds' Number
30%
Tip leakage flow
30%
Trailing Edge
29%
Reynolds-Averaged Navier-Stokes
28%
High-Pressure Turbine
28%
Gas Turbine Engine
28%
Preliminary Design Phase
27%
Preliminary Design
26%
Aerodynamics
25%
Nanoparticle
24%
Computer Simulation
23%
Propeller
22%
Broadband Noise
22%
Boundary Layer
21%
Numerical Study
19%
Numerical Analysis
19%
Leading Edge
18%
Aviation
18%
Shear Layer
17%
Derivative Gas Turbine
17%
Rotor Blade
17%
Mach Number
17%
Serration
16%
Analytical Model
16%
Preliminary Analysis
16%
Wall-Pressure
16%
Finite Volume
16%
Wind Tunnels
16%
Airport
15%
Maximum Lift Coefficient
15%
Optical Spectrum
15%
Design System
15%
Design Process
15%
Suction Side
14%
Experimental Result
14%
Flow Solver
14%
Mathematical Model
14%
Mathematical Modeling
14%
Nanocomposite
14%
Dilution
13%
Turbulent Flow
13%
Fluid Viscosity
12%
Noise Level
12%
Pressure Side
12%
Flat Plate
12%
Single Output
12%
Flow Velocity
11%
Low Flow Rate
11%
Direct Numerical Simulation
11%
Ground Level
11%
Recurrent Neural Network
11%
Output Parameter
11%
Helicopter Rotors
11%
Design Time
11%
Disc Turbine
11%
Input Multiple
11%
Vorticity
11%
Icephobic Coating
11%
Delamination
11%
Computer Aided Design
11%
Noise Contribution
11%
Angle-of-Attack
11%
Power Generation
11%
Air Quality
10%
Accident Prevention
10%
Simulation Result
10%
Flow Rate
10%
Numerical Method
10%
Comparative Study
10%
Mathematical Method
10%
Condensation
10%
Roughness Parameter
9%
Experimental Measurement
9%
Auxiliary Power Unit
9%
Equivalent Sand-Grain Roughness
9%
Velocity Profile
9%
Finite Element Analysis
9%
Boundary Condition
9%
Takeoff
9%
Parameterized Model
9%
Dynamic mode decomposition
9%
Navier-Stokes Equation
9%
Polymer
9%
Numerical Approach
8%
Flow Distribution
8%
Ice Crystal
8%
Cartesian Grid
8%
Level Set
8%
Turbulent Boundary Layer
8%