Flow visualization and computational studies of a reverse flow circular combustorThe development of a reverse-flow circular combustor is described in terms of the visualization techniques that are employed to optimize the flow and mixing of fuel and air. The Fluent computer program is used in conjunction with flow visualization studies to investigate the performance of the combustor. The combustor has multiple mini-combustion zones (MCZs) and fuel injection nozzles along its circular geometry, and the fuel injection design is modeled to determine temperature distribution, including the performance at the combustor exit. The yellow dye smoke used in the visualization demonstrated desirable flow patterns with rapid circulation patterns within the MCZs and extensive interaction between the channel flow and the MCZs. The results are similar to those of CFD models, and the main conclusions are that fuel atomization can be further optimized and that the fuel injector nozzle can control swirls, fuel spray angle, and jet penetration.
Document ID
19910064343
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ghorashi, B. (Cleveland State Univ. OH, United States)
Reardon, F. (Cleveland State Univ. OH, United States)
Mcbeath, G. (Cleveland State University OH, United States)
Chun, K. (NASA Lewis Research Center; Cleveland State University OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Heat Transfer and Fluid Mechanics Institute