Studies of High-Pressure Acoustic Combustion Instabilities in Hydrocarbon-Oxygen Liquid-Propellant RocketEngines Based on Reduced Chemical-Kinetic Mechanisms
Abstract
The objective is to conduct a collaborative research that will combine experimental measurements of methane-oxygen systems with numerical and modeling efforts to advance fundamental knowledge pertaining to the interplay of the acoustic field with the reactive flow in hydrocarbon-fueled liquid-propellant rocket engines, enabling the development of advanced modeling tools for predicting the instability behavior.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Jul 15, 2016
- Source ID
- FA95501610321
Entities
People
- Antonio Sanchez
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of California, San Diego