Keyphrases
De-icing
50%
Airfoil
49%
Heat Transfer
44%
Ice Accretion
41%
Icing
38%
Aircraft De-icing
35%
Ice Shape
34%
In-flight Icing
27%
Anti-icing System
27%
Penalization
27%
Computational Fluid Dynamics
25%
Numerical Simulation
25%
Ice Accretion Model
24%
Boundary Layer
21%
Simulation Code
19%
Numerical Results
18%
Anti-icing
18%
Reynolds number
17%
Turbulence Model
17%
Convective Heat Transfer
16%
Flat Plate
16%
Flow Solver
16%
Ice Shedding
16%
Microphysics
15%
Mathematical Model
15%
Three-dimensional (3D)
14%
Trajectory Calculation
14%
Rough Surface
14%
Surface Roughness
14%
Droplet Impingement
14%
Simulation System
14%
Impingement
13%
Maximum Lift Coefficient
13%
Sidewall
13%
Trisonic Wind Tunnel
13%
Wall Correction Factor
13%
Roughness Parameters
13%
Numerical Investigation
13%
Partial Differential Equations
13%
Icing Process
12%
Heat Load
12%
Cartesian Grid
11%
NACA 0012
11%
Navier-Stokes Equations
11%
Heat Transfer Prediction
11%
Correction Model
11%
Hot Air Anti-icing System
11%
Stall
11%
Blade Element Momentum Theory
10%
Nanoparticle Transport
10%
Engineering
Computational Fluid Dynamics
100%
Airfoil
71%
Snow and Ice Removal
65%
Ice Accretion
64%
Boundary Layer
30%
Jet
29%
Experimental Result
26%
Navier-Stokes Equation
23%
Simulation System
23%
Vortex
23%
Wind Tunnels
20%
Rotors
20%
Mathematical Model
19%
Flow Solver
18%
Simulation Code
18%
Roughness Parameter
16%
Partial Differential Equation
15%
Convective
15%
Cartesian Grid
15%
Level Set
15%
Flat Plate
15%
Thermal Load
14%
Reynolds-Averaged Navier-Stokes
14%
Reynolds' Number
13%
Nanoparticle
13%
Boundary Condition
13%
Equivalent Sand-Grain Roughness
12%
Maximum Lift Coefficient
12%
Side Wall
11%
Performance Degradation
11%
Roughness Effect
11%
Helicopter Rotors
11%
Air Flow
10%
Blade Element Momentum Theory
10%
Integral Method
10%
Heat And Mass Transfer
10%
Two Dimensional
9%
Lattice Method
9%
Angle-of-Attack
9%
Experimental Investigation
9%
Flow Condition
8%
Test Setup
8%
Numerical Study
8%
Numerical Method
8%
NASA
8%
3d Simulation
8%
Good Agreement
8%
Lift Coefficient
8%
Aerodynamic Force
8%
Internal Flow
8%
