Keyphrases
Hypersonic
77%
Thermal Non-equilibrium
50%
Mach number
48%
Hypersonic Flow
48%
Free Stream
46%
Direct numerical Simulation
45%
Global Stability Analysis
44%
Numerical Simulation
43%
Double Cone
38%
Global Instability
35%
Compression Corner
34%
State-specific
31%
Compression Ramp
31%
Boundary Layer
30%
Hypersonic Boundary Layer
29%
Two Dimensional
29%
Corner Flow
28%
Non-equilibrium
25%
Numerical Investigation
25%
Flow Field
25%
Separation Bubble
24%
Span-wise
24%
Dissociation
23%
Resolvent Analysis
21%
High Enthalpy
21%
Supersonic Flow
20%
Vibrational Excitation
20%
Two-temperature Model
20%
Unstable Modes
19%
Separation Region
19%
Unit Reynolds number
19%
Boundary Layer Interaction
17%
Non-equilibrium Simulations
17%
Ramp Angle
17%
Laminar Flow
17%
Coupling Model
16%
Computational Fluid Dynamics
16%
Streamwise Streaks
16%
Global Stability
15%
Reattachment
15%
Total Enthalpy
14%
Nozzle
14%
Laminar Boundary Layer
14%
Flat Plate
14%
Thermochemical Nonequilibrium Flows
13%
Reynolds number
13%
Shock-induced
13%
Low-frequency Unsteadiness
13%
Three-dimensional (3D)
12%
NavierStokes
12%
Engineering
Nonequilibrium
100%
Boundary Layer
62%
Stability Analysis
60%
Global Stability
59%
Direct Numerical Simulation
52%
Hypersonic Flows
48%
Reynolds' Number
42%
Computer Simulation
40%
Two Dimensional
37%
Mach Number
36%
Compression Corner
35%
Separation Bubble
29%
Layer Interaction
28%
Streamwise
27%
Heat Flux
24%
Separation Region
23%
Resolvent
23%
Vortex
22%
Computational Fluid Dynamics
21%
Supersonic Flow
20%
Reattachment
20%
Temperature Model
19%
Numerical Study
19%
Leading Edge
17%
Energy Engineering
17%
Laminar Flows
17%
Laminar Boundary Layer
15%
Free-Stream Mach Number
15%
One Dimensional
14%
Flat Plate
14%
Base Flow
14%
Flow Structure
13%
Oscillatory
13%
Test Condition
12%
Turbulent Flow
12%
Turbulent Boundary Layer
12%
Flow System
12%
Free-Stream Condition
11%
Axisymmetric
11%
Vibrational Relaxation
10%
Nanosecond
10%
External Disturbance
10%
Mode Dynamic
10%
Dimensionality
10%
Shear Layer
10%
Separated Flow
10%
Pressure Fluctuation
9%
Air Condition
9%
Transients
9%
Quasi Steady State
9%