Molecular Dynamics Simulations of Supercritical Jet Mixing
PENNSYLVANIA STATE UNIV UNIVERSITY PARK DEPT OF AEROSPACE ENGINEERING
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High pressure heterogeneous combustion systems typically operate trans- or supercritical Liquid rocket engines Gas turbine combustors andor Diesel engines. Quantitative assessments or validated theories characterizing propellant injection at near and supercritical conditions are currently limited.
- Fluid Mechanics
- Atomic and Molecular Physics and Spectroscopy