Engineering
Computational Fluid Dynamics
100%
Vortex
67%
Separation Bubble
61%
Powder Injection
58%
Injection Moulding
58%
Actuator Line Method
58%
Compressed Air Motors
55%
Actuator Disk
45%
Reynolds Stress
42%
Jet
39%
Rotors
35%
Turbine
33%
Actuator
31%
Wall-Pressure
29%
Pressure Fluctuation
29%
Experimental Investigation
29%
Orifice
29%
Mold Filling
29%
Diesel Fuel
29%
Internal Flow
29%
Hydrodynamics
29%
Navier-Stokes Equation
28%
Experimental Result
26%
Turbulent Flow
25%
Dynamic Model
25%
Simulation Result
24%
Side Wall
24%
Reattachment
24%
Flow Structure
24%
Numerical Model
24%
Porosity
24%
Injection Pressure
24%
Boundary Layer
22%
Discretization
21%
Fluid Viscosity
21%
Numerical Method
21%
Flow Dynamics
21%
Reynolds-Averaged Navier-Stokes
21%
Coherent Structure
21%
Velocity Fluctuation
20%
Vortex System
19%
Moldflow
19%
Wind Power
19%
Streamwise
19%
Turbulence Intensity
19%
Control System
18%
Proper Orthogonal Decomposition
18%
Stainless Steel
17%
Binder System
17%
Direct Numerical Simulation
17%
Keyphrases
Large Eddy Simulation
79%
Turbulence
78%
Turbulent Separation
62%
Separation Bubble
62%
Actuator Disc
52%
Pressure-induced
51%
Actuator Line Method
48%
Diesel Injector
43%
Low Pressure Injection Molding
43%
Wind Turbine
38%
Wake Vortex
38%
Needle Lift
37%
Sac Volume
36%
Near Wake
31%
Single Orifice
29%
Metallic Feedstock
29%
CFD Study
29%
Numerical Simulation
27%
Injection Pressure
26%
Computational Fluid Dynamics
26%
Needle Motion
26%
Wall Pressure Fluctuations
25%
Reattachment
24%
Turbulence Model
24%
Vol%
24%
Navier-Stokes Equations
23%
Actuator Line
22%
Internal Flow
22%
Streamwise
22%
Powder Injection Molding
21%
Wind Farm
21%
Mold Filling
21%
OpenFOAM
21%
Coherent Structures
21%
Stainless Steel Powder
20%
Binder System
20%
Sidewall
20%
Velocity Fluctuation
20%
Flow Dynamics
19%
Span-wise
19%
Vortex Tube
19%
Numerical Methods
19%
Vortex Method
19%
Turbulent Flow
18%
Proper Orthogonal Decomposition
18%
Reynolds-averaged Navier-Stokes Model
18%
Direct numerical Simulation
17%
Injector Flow
17%
Reynolds Stress
17%
Divergence-free
16%