High Fidelity Modeling and Simulation of Supercritical Turbulent Combustion
Abstract
There are three objectives for this proposal: 1) the high fidelity modeling and simulation capability for supercritical mixing and combustion at conditions typically encountered in aerospace propulsion engines. 2) to develop subgrid models using trans-critical, vapor-liquid equilibrium approach for supercritical turbulence- chemical kinetics interactions, including in situ co-processing, online data analysis, science-driven orchestration of data analytics and multi-threaded acceleration strategies 3) investigate Theoretically investigations to identify the transition between multi-phase and single-phase interface dynamics in multicomponent fluids at supercritical pressures to develop closure for turbulent transport and combustion of real-fluid mixtures based on space-time filtering
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Apr 09, 2018
- Source ID
- FA95501810216
Entities
People
- Vigor Yang
Organizations
- Air Force Office of Scientific Research
- Georgia Tech Research Corporation
- United States Air Force