Turbulent Flame Structure of Cavity Stabilized Reacting Shear Layers: Effects of Flow Compressibility, Heat Release, and Finite-rate Kinetics
Abstract
The objective of this proposal is to study the compressibility and heat release effects on turbulent flame structure and stabilization mechanisms, especially for high-speed reacting shear flow over cavity. Fundamental data on flame structure and statistics on key species are to be obtained experimentally. Computational results using DNS will supplement the experiments to provide additional information not accessible from experiments in developing submodels.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA95501510440
Entities
People
- Harsha Chelliah
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of Virginia