Engineering
Boundary Layer
100%
Direct Numerical Simulation
94%
Large Eddy Simulation
93%
Shear Layer
78%
Reduced Order Model
72%
Boundary Condition
69%
Turbulent Boundary Layer
57%
Two Dimensional
48%
Actuation
40%
Mach Number
39%
Compressible Navier
39%
Duct
39%
Computer Simulation
38%
Orifice
35%
Axisymmetric
35%
Layer Interaction
34%
Inductively Coupled Plasma
34%
Mixing Layer
33%
Discretization
32%
Mode Dynamic
31%
Acoustic Field
31%
Sound Source
29%
Ignition
28%
Thermal Fluid
28%
Finite Element Method
27%
Pressure Fluctuation
26%
Global Mode
26%
Computational Fluid Dynamics
26%
Energy Engineering
25%
Navier-Stokes Equation
25%
Reynolds' Number
24%
NASA
23%
Term Approximation
23%
Incident Sound
22%
Sound Pressure Level
22%
Flow Condition
21%
Supercharger
21%
Momentum Equation
21%
Time Domain
20%
Harmonics
20%
Sound Field
20%
Material Response
18%
Thermal Protection
18%
System Protection
18%
Laminar Boundary Layer
18%
Structured Mesh
17%
Circular Aperture
17%
Elastic Plate
17%
Sound Generation
17%
Control Flow
17%
Keyphrases
Direct numerical Simulation
93%
Large Eddy Simulation
73%
Turbulent Boundary Layers
59%
Reduced Order Model
58%
Acoustics
50%
Boundary Layer
47%
Turbulent Jet
43%
Three-dimensional (3D)
40%
Aeroelastic Response
39%
Hypersonic
38%
High-speed Jet
37%
Acoustic Liner
37%
Jet Noise
36%
Overset Grid
35%
Piston Theory
35%
Shear Layer
34%
Honeycomb Liner
34%
Actuator
34%
Grazing Flow
34%
Two Dimensional
34%
Flow Field
32%
Mean Flow
32%
Liner
32%
Simultaneous Approximation Terms
31%
Fluid-structure Interaction
31%
Mach number
31%
Noise Reduction
31%
High-order
30%
Dynamic Mode Decomposition
29%
Acoustic Response
28%
Turbocharger
28%
Acoustic Field
28%
Ignition
26%
Compressible Navier-Stokes
26%
Actuation
25%
Numerical Simulation
25%
Numerical Investigation
25%
Shock Wave Boundary Layer Interaction
25%
Aeroacoustics
24%
Orifice
23%
Sensor Placement
23%
Plasma Actuator
23%
Global Modes
23%
Complex Geometry
22%
Material Response
21%
Turbulence
21%
Adjoint-based Optimization
20%
Mixing Layer
20%
Thermal Protection System
19%
Flow Condition
18%