DETAILED SIMULATION AND MODELING OF TURBULENT MULTISCALAR MIXING AND COMBUSTION PROCESSES AT SUPERCRITICAL CONDITIONS
Abstract
The objective is to develop hybrid Direct Numerical and Large Eddy simulation to reduce the barriers that are hindering the development of advanced predictive models for liquid rocket engines, via high-fidelity models for turbulent reacting flows at supercritical conditions. The goal is to develop accurate physics-based predictive modeling, identification and management of errors and uncertainties, and effective utilization of next generation supercomputers, to design the future combustion systems.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Aug 12, 2021
- Source ID
- FA95502010185
Entities
People
- Vigor Yang
Organizations
- Air Force Office of Scientific Research
- Georgia Tech Research Corporation
- United States Air Force