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Keyphrases
Airfoil
90%
Large Eddy Simulation
82%
De-icing
72%
Dielectric Properties
55%
Noise Prediction
49%
Polyethylene
49%
Aircraft Engine
46%
Microphysics
45%
Polystyrene
45%
Contrails
45%
Reynolds number
43%
Near-field
42%
Few-layer Graphene
41%
Heat Transfer
40%
Tip Gap
39%
Ice Accretion
39%
Noise Source
39%
Contrail Formation
38%
Graphene
38%
Broadband Noise
37%
Noise Generation Mechanism
35%
Tip Leakage Vortex
33%
Direct numerical Simulation
32%
Rheological Properties
32%
Reynolds-averaged Navier-Stokes
31%
Surface Roughness
31%
Electrical Properties
30%
Numerical Simulation
30%
Tip Leakage Flow
30%
Installation Effects
29%
Soot
29%
Gas Turbine Engine
29%
Preliminary Design Phase
27%
Graphene Nanoplatelets
26%
Tip Noise
26%
Soot Particles
26%
Propeller
25%
Analytical Model
25%
Aircraft De-icing
25%
Penalization
24%
Trailing Edge Noise
24%
Icing
24%
Rotor
24%
Photodegradation
24%
Shear Layer
24%
Mach number
24%
High-density Polyethylene
23%
High-pressure Turbine
23%
Serration
23%
Airport
23%
Computational Fluid Dynamics
23%
Operating Conditions
22%
Polypropylene
22%
Ice Shedding
22%
Mechanical Properties
21%
Commercial Graphene
21%
Clay
21%
Rheological Behavior
20%
Nanoparticle Dispersion
20%
Three-dimensional (3D)
20%
Numerical Investigation
20%
Ice Accretion Simulation
19%
Far-field Noise
19%
Plume
19%
Fuel Sulfur Content
19%
Airfoil Noise
19%
Anti-icing
18%
Aeroderivative Gas Turbine
18%
Rotor Blade
18%
Nanoparticles
18%
Vortex
18%
Ice Crystals
18%
Butylenes
18%
Thermoplastic Elastomer
18%
Commercial Aircraft
17%
Aerosol Formation
17%
Maximum Lift Coefficient
17%
Turbulent Boundary Layers
17%
Adverse Pressure Gradient
17%
NARX Model
17%
Ducted Tail Rotor
17%
Molecular Dynamics
17%
Linear Low-density Polyethylene (LLDPE)
17%
Polyamide 1010
17%
Styrenic Block Copolymers
17%
Electrical Conductivity
17%
Flow Solver
17%
Eulerian
17%
Nanofillers
17%
Hexagonal Boron Nitride (h-BN)
16%
RANS Simulation
16%
Graphene Oxide
16%
Acoustics
16%
Flat Plate
16%
Wall Pressure
16%
Microphysical Model
16%
Wind Tunnel
16%
Flow around
16%
Turbulence Model
16%
Aerofoil
16%
Engineering
Airfoil
100%
Aircraft
99%
Computational Fluid Dynamics
84%
Large Eddy Simulation
81%
Snow and Ice Removal
63%
Rotors
56%
Ice Accretion
49%
Jet
44%
Aircraft Engine
38%
Noise Source
35%
Tip leakage flow
34%
Reynolds' Number
33%
Trailing Edge
31%
Reynolds-Averaged Navier-Stokes
31%
High-Pressure Turbine
29%
Gas Turbine Engine
29%
Preliminary Design Phase
28%
Aerodynamics
28%
Preliminary Design
27%
Nanoparticle
25%
Propeller
23%
Computer Simulation
23%
Broadband Noise
23%
Numerical Study
22%
Numerical Analysis
22%
Aviation
22%
Good Agreement
22%
Boundary Layer
20%
Leading Edge
20%
Experimental Result
19%
Airport
19%
Mach Number
19%
Shear Layer
18%
Derivative Gas Turbine
18%
Serration
17%
Analytical Model
17%
Preliminary Analysis
17%
Finite Volume
17%
Roughness Parameter
16%
Maximum Lift Coefficient
16%
Design System
15%
Design Process
15%
Optical Spectrum
15%
Flow Solver
15%
Mathematical Model
15%
Mathematical Modeling
15%
Air Quality
14%
Dilution
14%
Turbulent Flow
14%
Wind Tunnels
14%
Condensation
13%
Suction Side
13%
Flow Velocity
13%
Low Flow Rate
12%
Numerical Prediction
12%
Noise Level
12%
Pressure Side
12%
Flat Plate
12%
Single Output
12%
Rotor Blade
12%
Simulation Result
12%
Nanocomposite
11%
Wall-Pressure
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%
Experimental Measurement
11%
Flow Rate
11%
Computer Aided Design
11%
Noise Contribution
11%
Angle-of-Attack
11%
Power Generation
11%
Accident Prevention
11%
Parametric Study
11%
Fluid Viscosity
11%
Numerical Method
10%
Comparative Study
10%
Auxiliary Power Unit
10%
Equivalent Sand-Grain Roughness
10%
Velocity Profile
10%
Finite Element Analysis
9%
Boundary Condition
9%
Takeoff
9%
Parameterized Model
9%
Gas Turbine
9%
Dynamic mode decomposition
9%
Navier-Stokes Equation
9%
Numerical Approach
9%
Flow Distribution
9%
Ice Crystal
9%
Cartesian Grid
8%
Level Set
8%
Turbulent Boundary Layer
8%
Boltzmann Equation
8%
Nusselt Number
8%