Keyphrases
Argon
10%
Atomic Oxygen
10%
Bhatnagar-Gross-Krook
8%
Boundary Layer
6%
Bow Shock
20%
Chemistry Model
8%
Collision Energy
7%
Condensation
14%
Condensing Flow
7%
Direct Simulation Monte Carlo
89%
Dissociation
8%
Double Cone
7%
Double Wedge
7%
DSMC Method
7%
DSMC Simulation
7%
Electrospray
11%
Flow Condition
6%
Flow Field
22%
Free Stream
9%
High Altitude
19%
Homogeneous Condensation
11%
Hypersonic
26%
Hypersonic Flow
28%
Hypersonic Non-equilibrium Flow
7%
Hypersonic Re-entry
11%
Ion Thruster Plume
11%
Ionic Liquid
9%
Kinetic Approach
7%
Kinetic Model
9%
Mach number
6%
Micronozzle
6%
Molecular Dynamics
27%
Molecular Dynamics Simulation
15%
Monte Carlo Method
11%
Monte Carlo Simulation
11%
Nitric Oxide
6%
Non-equilibrium
10%
Number Density
8%
Numerical Simulation
8%
Plume
40%
Quasi-classical Trajectory
8%
Reentry
7%
Reentry Flow
14%
Reynolds number
7%
Rocket
8%
Shock
26%
Shock Layer
8%
Stagnation Pressure
8%
Three-dimensional (3D)
8%
Thruster
12%
Engineering
Adaptive Mesh Refinement
6%
Aerodynamics
5%
Axisymmetric
12%
Boundary Condition
9%
Boundary Layer
17%
Bow Shock
20%
Cluster Size
7%
Computational Fluid Dynamics
10%
Computer Simulation
19%
Cross Section
11%
Direct Simulation
100%
Electric Field
8%
Electrospray
14%
Energy Engineering
25%
Excited State
5%
Flow Condition
5%
Flow Field
10%
Flow in Nozzles
7%
Flow Regime
5%
Free Expansion
5%
Gas Flow
7%
Good Agreement
14%
Heat Flux
7%
Hypersonic Flows
30%
Layer Interaction
7%
Mach Number
8%
Microelectromechanical System
6%
Monte Carlo Approach
8%
Multiscale
9%
Nonequilibrium
27%
Number Density
9%
One Dimensional
7%
Quasi Steady State
5%
Reynolds' Number
10%
Rotational
11%
Shock Interaction
5%
Shock Layer
8%
Simulation Result
6%
Spatial Distribution
6%
Stagnation Pressure
9%
System Protection
5%
Thermal Protection
6%
Thruster
29%
Two Dimensional
5%
