1.6. Rocket and Jet Propulsion
Small Scale Jet Propulsion System (PDE) Analysis by All Eulerian Method Governing equations - - 2D cylindrical compressible reactive Navier-Stokes equations (Fluid)
- - Mie-Gruneisen EOS with Johnson-Cook model with modified Navier-Stoke equations (Solid)
- - Level set method based on ghost fluid method (Interface)
Simulation - - Detonation, elasto-plastic deforming (for validation), and pulse detonation engine (PDE)
 | | Fig. Kerosene detonation modeling (Detonation cell) | Fig. Detonation with elasto-plastic deformed tube |  | | Fig. Rigid and elastic vibrating wall of PDE simulation | Fig. Schematic diagram of Kerosene PDE | Rocket Launching System Analysis using Strongly Coupled FSI Method Governing equations - - 2D compressible reactive Navier-Stokes equations (Fluid)
- - Total Lagrangian model (Solid)
- - Level set method based on ghost fluid method (Interface)
Analysis - Navy’s vertical launching system  | | Fig. Shadowgraph (gray) and temperature (color) contour |  | | Fig. Vertical Launching System | | 
