Effects of Injection Initial Conditions and Length-to-Diameter Ratio on Fuel Propulsive Droplets Sizing in a Duct

Author:

Doustdar Mohammad Mahdi1,Mojtahedpoor Mohammad2,Wadizadeh Mohammad1

Affiliation:

1. Imam Hossein University

2. Imam Hossein University of Tehran

Abstract

In this paper an empty cylinder which is as a simulator for a ramjet engine has been studied by a cold flow. The air flow comes into the cylinder from one side and injection operation will be done by four nozzles which are located in the entrance of cylinder. By changing length to diameter ratio and injection angle, we have studied droplet sizing and efficient mass fraction of fuel vapor near and at the exit area. We named the mass of fuel vapor inside the flammability limit as the efficient mass fraction. To fulfill the calculation we used a modified version of KIVA-3V.

Publisher

Trans Tech Publications, Ltd.

Reference11 articles.

1. KIVA-II: A Computer Program for Chemically Reactive Flows with Sprays, Los Alamos, National laboratory.

2. S. R. Turns, An introduction to Combustion Concepts and Applications, Second edition, Chapter 10 , 369-410 (2000).

3. G. L. Hubbard, V. E. Denny and A. F. Mills, Droplet Evaporation: Effects of Transiments and Variable Properties, University of California, Los Angeles, CA 90024, U.S. A.

4. F. R. Newbold and N. R. Amundson. A model for evaporation of a multi-component droplet, A.Z. Ch.E. JI, 19, 22-30 (1973).

5. K. Prommersberger, G. Maier, S. Wittig, Validation and Application of a Droplet Evaporation Model for Real Aviation Fuel.

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