1992-08-03

Parameter Effects on Turbulent Swirling Flames in Combustors 929225

A computer code has been developed to simulate the turbulent combustion flowfield of an axisymmetric swirling flow in a typical combustor. Premixed fuel (methane) and air enter the combustor through the main primary inlet. Additionally, a top wall secondary annular inlet is permitted through which cooling dilution air flows. Once the geometric sizes of the domain and inlets are specified parameters of interest include the primary fuel-air ratio and aerodynamic specification of all the inflows. This includes the secondary to primary velocity ratio, primary swirl and contraction angles, and secondary swirl and upstream angles. Combustion flowfield predictions are given to illustrate the effects of these parameters on the flowfield (velocities, species concentrations, temperature and turbulence levels), and dramatic effects are illustrated via radial profiles and streamline patterns.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 17% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Developing a Fuel Stratification Concept on a Spark Ignition Engines

2007-01-0476

View Details

TECHNICAL PAPER

Concept of Lean Combustion by Barrel-Stratification

920678

View Details

TECHNICAL PAPER

A Study About In-Cylinder Flow and Combustion in a 4-Valve S.I. Engine

920574

View Details

X