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Keyphrases
Adverse Pressure Gradient
18%
Aeroderivative Gas Turbine
19%
Aerofoil
16%
Aerosol Formation
18%
Aircraft De-icing
25%
Aircraft Engine
46%
Airfoil
85%
Airfoil Noise
19%
Airport
24%
Analytical Model
25%
Anti-icing
19%
Broadband Noise
37%
Butylenes
18%
Cartesian Grid
16%
Clay
21%
Commercial Aircraft
18%
Commercial Graphene
22%
Computational Fluid Dynamics
23%
Contrail Formation
39%
Contrails
45%
De-icing
73%
Design Process
16%
Dielectric Properties
56%
Direct numerical Simulation
32%
Ducted Tail Rotor
18%
Electrical Conductivity
17%
Electrical Properties
31%
Eulerian
17%
Far-field Noise
18%
Few-layer Graphene
42%
Flow around
16%
Flow Solver
17%
Fuel Sulfur Content
19%
Gas Turbine Engine
29%
Graphene
39%
Graphene Nanoplatelets
27%
Graphene Oxide
17%
Heat Transfer
40%
Hexagonal Boron Nitride (h-BN)
17%
High-density Polyethylene
24%
High-pressure Turbine
24%
Ice Accretion
39%
Ice Accretion Simulation
20%
Ice Crystals
18%
Ice Shedding
22%
Icing
24%
Installation Effects
30%
Large Eddy Simulation
76%
Linear Low-density Polyethylene (LLDPE)
18%
Mach number
22%
Maximum Lift Coefficient
18%
Mechanical Properties
22%
Microphysical Model
17%
Microphysics
46%
Molecular Dynamics
18%
Nanofillers
17%
Nanoparticle Dispersion
21%
Nanoparticles
18%
NARX Model
18%
Near-field
42%
Noise Generation Mechanism
34%
Noise Prediction
50%
Noise Source
37%
Numerical Investigation
20%
Numerical Simulation
28%
Operating Conditions
23%
Penalization
25%
Photodegradation
24%
Plume
19%
Polyamide 1010
18%
Polyethylene
49%
Polypropylene
22%
Polystyrene
45%
Preliminary Design Phase
28%
Propeller
26%
RANS Simulation
17%
Reynolds number
42%
Reynolds-averaged Navier-Stokes
31%
Rheological Behavior
21%
Rheological Properties
32%
Rotor
24%
Rotor Blade
18%
Serration
24%
Shear Layer
24%
Soot
29%
Soot Particles
27%
Styrenic Block Copolymers
18%
Surface Roughness
31%
Thermoplastic Elastomer
18%
Three-dimensional (3D)
20%
Tip Gap
34%
Tip Leakage Flow
24%
Tip Leakage Vortex
32%
Tip Noise
25%
Trailing Edge Noise
24%
Turbulence Model
16%
Turbulent Boundary Layers
18%
Vortex
18%
Wall Pressure
17%
Wind Tunnel
16%
Engineering
Accident Prevention
11%
Aerodynamics
26%
Air Quality
14%
Aircraft
100%
Aircraft Engine
38%
Airfoil
94%
Airport
20%
Analytical Model
18%
Angle-of-Attack
11%
Auxiliary Power Unit
10%
Aviation
22%
Boltzmann Equation
9%
Boundary Condition
10%
Boundary Layer
21%
Broadband Noise
23%
Cartesian Grid
9%
Comparative Study
11%
Computational Fluid Dynamics
85%
Computer Aided Design
12%
Computer Simulation
22%
Condensation
13%
Derivative Gas Turbine
19%
Design Process
16%
Design System
16%
Design Time
12%
Dilution
14%
Direct Numerical Simulation
12%
Disc Turbine
12%
Dynamic mode decomposition
10%
Equivalent Sand-Grain Roughness
10%
Experimental Measurement
12%
Experimental Result
20%
Finite Element Analysis
10%
Finite Volume
17%
Flat Plate
11%
Flow Distribution
9%
Flow Rate
12%
Flow Solver
15%
Flow Velocity
13%
Fluid Viscosity
11%
Gas Turbine
10%
Gas Turbine Engine
30%
Good Agreement
20%
Ground Level
12%
Helicopter Rotors
12%
High-Pressure Turbine
30%
Ice Accretion
50%
Ice Crystal
9%
Input Multiple
12%
Jet
45%
Large Eddy Simulation
76%
Leading Edge
20%
Level Set
9%
Low Flow Rate
13%
Mach Number
18%
Mathematical Model
15%
Mathematical Modeling
15%
Maximum Lift Coefficient
16%
Nanocomposite
12%
Nanoparticle
25%
Navier-Stokes Equation
9%
Noise Contribution
12%
Noise Level
11%
Noise Source
31%
Numerical Analysis
22%
Numerical Approach
9%
Numerical Method
11%
Numerical Prediction
13%
Numerical Study
22%
Nusselt Number
9%
Optical Spectrum
15%
Output Parameter
12%
Parameterized Model
10%
Parametric Study
11%
Power Generation
11%
Preliminary Analysis
18%
Preliminary Design
28%
Preliminary Design Phase
29%
Pressure Side
11%
Propeller
24%
Recurrent Neural Network
12%
Reynolds' Number
32%
Reynolds-Averaged Navier-Stokes
31%
Rotor Blade
12%
Rotors
56%
Roughness Parameter
16%
Serration
18%
Shear Layer
19%
Simulation Result
12%
Single Output
12%
Snow and Ice Removal
64%
Suction Side
12%
Takeoff
10%
Tip leakage flow
29%
Trailing Edge
30%
Turbulent Boundary Layer
9%
Turbulent Flow
14%
Velocity Profile
10%
Wall-Pressure
12%
Wind Tunnels
14%