Keyphrases
Navier-Stokes
87%
Three-dimensional (3D)
83%
Two-phase Flow
75%
Stokes Method
75%
Nozzle Exit
50%
Dual-time
45%
Gas Field
37%
Computational Fluid Dynamics
37%
Fluid Flow Characteristics
37%
Local Volume Fraction
37%
Implicit Algorithm
37%
Two Dimensional
37%
Parallel Execution
37%
Well Conditions
37%
Eigenvalues
37%
Non-condensable Gas
37%
Eigensystem
37%
Computational Efficiency
37%
Time Derivative
37%
Navier-Stokes Equations
37%
Volume Fraction
37%
Special Care
37%
Cavitating
37%
High-density Ratio
37%
System of Differential Equations
37%
Implicit Method
37%
Computational Aeroacoustics
35%
Rectangular Jet
33%
Exit Conditions
33%
High-order Accurate
33%
Numerical Prediction
33%
Turbulence
32%
Reynolds-averaged Navier-Stokes Equations
30%
Half Step
29%
Dynamic Control
25%
Current Control
25%
Corner Vortex
25%
Design Test
25%
Piping System
25%
Noise Source
25%
Air Transport
25%
Control Characteristics
25%
Recommender Systems
25%
Control Efficacy
25%
Distilling
25%
Fighter
25%
Equation-based
25%
Collision Term
25%
Boltzmann Model Equation
25%
Bhatnagar-Gross-Krook
25%
Engineering
Computational Fluid Dynamics
100%
Two-Phase Flow
75%
Density Ratio
75%
Reynolds-Averaged Navier-Stokes
67%
Non-Condensable Gas
45%
Dual Time
45%
Gas Field
45%
Eigenvalue
37%
Two Dimensional
37%
Turbulence Intensity
37%
Flat Plate Boundary Layer
37%
Implicit Method
37%
Computational Efficiency
37%
Fluid Flow Characteristic
37%
Fourth Order
33%
Grid Point
33%
Kirchhoff
33%
Sixth Order
33%
Central Difference
33%
Turbulent Flow
25%
Hulls (Ship)
25%
Newtonian Fluid
25%
Computational Resource
25%
Selection Algorithm
25%
Air Transport
25%
Noise Source
25%
Static Stability
25%
Fighter Aircraft
25%
Piping Systems
25%
Good Performance
25%
Ducted Fan
25%
Circular Cylinder
25%
Applicability
25%
Element Basis
25%
Test Data
25%
Tunnel
25%
Parallel Computer
25%
Skin Friction Drag
25%
Nozzle Exit
25%
Drag Reduction
25%
Flat Plate
25%
Numerical Prediction
25%
Performance Improvement
25%
Induced Drag
25%
Collision Term
25%
