Numerical Simulation of Gel Propellant Droplet Breakup in Airflow

Volume: 232, Pages: 502 - 507
Published: Nov 1, 2012
Abstract
The droplet breakup is of importance in variety of spay combustion field. In order to investigate gel propellant droplet breakup in a gaseous phase, the Navier-Stokes equations in their axi-symmetric form was solved using the finite volume technique, and the Volume of Fluid method (VOF) was employed for tracking the free liquid-gas interface during process of droplet breakup. The results were compared with available published experimental data...
Paper Details
Title
Numerical Simulation of Gel Propellant Droplet Breakup in Airflow
Published Date
Nov 1, 2012
Volume
232
Pages
502 - 507
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