High pressure heterogeneous combustion systems typically operate trans- or supercritical: Liquid rocket engines; Gas turbine combustors; and/or Diesel engines. Quantitative assessments or validated theories characterizing propellant injection at near and supercritical conditions are currently limited.
Molecular Dynamics Simulations of Supercritical Jet Mixing
2004
27 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Physical & Theoretical Chemistry , High pressure , Diatomic molecules , Equations of state , Rocket engines , Simulation , Diesel engines , Experimental data , Propellants , Liquid rocket fuels , Combustion , Three dimensional , Symposia , Validation , Theory , Supercritical jet mixing , Component reports