Exploration of Acoustically Coupled Combustion Instabilities Relevant to Rocket Propulsion Systems
Abstract
The objective of this proposal is to investigate the combustion stability and flame dynamics of fuel droplets infused with nano particle substance additives and subjecting them to acoustic pressures in a controlled environment. This research will be directly linked to the AFRL RQRC intramural research titled “Dynamics of High Pressure Reacting Shear Flows”.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Jan 14, 2022
- Source ID
- FA95501910096
Entities
People
- Ann Karagozian
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of California, Los Angeles