Accession Number:

ADA446421

Title:

Molecular Dynamics Simulations of Supercritical Jet Mixing

Descriptive Note:

Conference paper

Corporate Author:

PENNSYLVANIA STATE UNIV UNIVERSITY PARK DEPT OF AEROSPACE ENGINEERING

Report Date:

2004-06-25

Pagination or Media Count:

27.0

Abstract:

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.

Subject Categories:

  • Fluid Mechanics
  • Atomic and Molecular Physics and Spectroscopy

Distribution Statement:

APPROVED FOR PUBLIC RELEASE