INIS
rocket engines
100%
start-up
100%
liquids
100%
computerized simulation
100%
transfer functions
50%
injection
50%
deposits
50%
dynamics
50%
levels
50%
parametric analysis
50%
distribution
50%
two-phase flow
50%
sprays
50%
numerical solution
50%
propellants
50%
droplets
50%
nozzles
50%
walls
50%
evaporation
50%
size
50%
experimental data
50%
combustion chambers
50%
iterative methods
50%
Engineering
Stage Rocket
100%
Lagrange
50%
Droplet Size
50%
Nozzle
50%
Computational Analysis
50%
Initial Temperature
50%
Combustion Chamber
50%
Flow Field
50%
Parametric Study
50%
Superheated Liquid
50%
Solution Technique
50%
Material Science
Temperature
100%
Liquid
100%
Nozzle
50%
Droplet
50%
Two Phase Flow
50%