Engineering
Acoustic Field
31%
Actuation
40%
Axisymmetric
35%
Boundary Condition
69%
Boundary Layer
100%
Circular Aperture
17%
Compressible Navier
39%
Computational Fluid Dynamics
26%
Computer Simulation
38%
Control Flow
17%
Direct Numerical Simulation
94%
Discretization
32%
Duct
39%
Elastic Plate
17%
Energy Engineering
25%
Finite Element Method
27%
Flow Condition
21%
Global Mode
26%
Harmonics
20%
Ignition
28%
Incident Sound
22%
Inductively Coupled Plasma
28%
Laminar Boundary Layer
18%
Large Eddy Simulation
93%
Layer Interaction
34%
Mach Number
39%
Material Response
18%
Mixing Layer
33%
Mode Dynamic
31%
Momentum Equation
21%
NASA
23%
Navier-Stokes Equation
25%
Orifice
35%
Pressure Fluctuation
26%
Reduced Order Model
68%
Reynolds' Number
23%
Shear Layer
78%
Sound Field
20%
Sound Generation
17%
Sound Pressure Level
22%
Sound Source
26%
Structured Mesh
17%
Supercharger
21%
System Protection
18%
Term Approximation
23%
Thermal Fluid
28%
Thermal Protection
18%
Time Domain
20%
Turbulent Boundary Layer
57%
Two Dimensional
46%
Keyphrases
Acoustic Field
28%
Acoustic Liner
37%
Acoustic Response
28%
Acoustics
50%
Actuation
25%
Actuator
34%
Adjoint-based Optimization
20%
Aeroacoustics
24%
Aeroelastic Response
39%
Boundary Layer
47%
Complex Geometry
22%
Compressible Navier-Stokes
26%
Direct numerical Simulation
93%
Dynamic Mode Decomposition
29%
Flow Condition
18%
Flow Field
32%
Fluid-structure Interaction
31%
Global Modes
23%
Grazing Flow
34%
High-order
30%
High-speed Jet
37%
Honeycomb Liner
34%
Hypersonic
38%
Ignition
26%
Jet Noise
36%
Large Eddy Simulation
73%
Liner
32%
Mach number
31%
Material Response
21%
Mean Flow
32%
Mixing Layer
20%
Noise Reduction
31%
Numerical Investigation
25%
Numerical Simulation
25%
Orifice
23%
Overset Grid
35%
Piston Theory
35%
Plasma Actuator
23%
Reduced Order Model
54%
Sensor Placement
23%
Shear Layer
34%
Shock Wave Boundary Layer Interaction
25%
Simultaneous Approximation Terms
31%
Thermal Protection System
19%
Three-dimensional (3D)
40%
Turbocharger
28%
Turbulence
21%
Turbulent Boundary Layers
59%
Turbulent Jet
43%
Two Dimensional
32%