학술논문
Unsteady flow phenomena in an axisymmetric combustor
Document Type
Conference
Author
Source
ICIASF 2001 Record, 19th International Congress on Instrumentation in Aerospace Simulation Facilities (Cat. No.01CH37215) Instrumentation in aerospace simulation facilities Instrumentation in Aerospace Simulation Facilities, 2001. 19th International Congress on ICIASF 2001. :59-69 2001
Subject
Language
Abstract
The unsteady flow characteristics prevailing in a simple axisymmetric combustor are described. Unexpected bimodal velocity distributions are present in various regions of the flow, which are not accounted for in mathematical models. Understanding and accurate modeling of such flow behavior is essential as it can significantly affect the fuel/air mixing process, thus impacting combustion efficiency and emissions.