Calculation of a hollow-cone liquid spray in a uniform air stream
Abstract
Fluid dynamic computer codes for the simulation of flows in gas turbine engine combustion systems are being developed. NASA is currently sponsoring a two-phase program for the evaluation of the performance of current codes, taking into account also an improvement of accuracy, if needed. The present investigation forms a part of this program. The numerical technique used includes a Lagrangian spray model for liquid fuels. The spray model, in conjunction with the turbulence model, determines the distribution of fuel in the burning zone of the combustor. The numerical technique was applied to a hollow-cone pressure atomizer spraying water into a coflowing confined airstream.
- Publication:
-
AIAA
- Pub Date:
- June 1984
- Bibcode:
- 1984jpco.confQ....S
- Keywords:
-
- Air Flow;
- Computational Fluid Dynamics;
- Flow Distribution;
- Fuel Sprays;
- Liquid Fuels;
- Uniform Flow;
- Boundary Value Problems;
- Cones;
- Drop Size;
- Flow Velocity;
- Liquid Atomization;
- Particle Trajectories;
- Stochastic Processes;
- Turbulence Models;
- Weibull Density Functions;
- Wind Tunnel Tests;
- Fluid Mechanics and Heat Transfer