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Virginia Polytechnic Institute and State University

Effect of inlet configurations on the aerodynamics of swirl combustors

Abstract

dc:description.abstract

The flowfield in a swirling combustor with a Confinement Ratio of 1.6 was simulated in water. Qualitative measurements were made from flow visualization in a horizontal water rig with the help of Pliolite beads and liquid dye. Velocity and turbulence measurements were made in a cold air flow rig. Mean velocity measurements were made using a five hole Pitot probe and turbulence measurements were obtained from a hot wire anemometer. All the flow visualization tests were made with Reynold's number between 10,000 and 47,500, and quantitative measurements in the cold air flow were made at a Reynold's number of 7.1x10<sup>5</sup>. The experiment was conducted for two configurations of the combustor system inlet- 1) Straight inlet and 2) S-inlet. Both configurations were tested with swirling and non-swirling flows. The straight inlet configuration with non-swirling flow produced a uniform corner recirculation near the wall of the combustion chamber. The S-inlet made the corner recirculation zones unequal. The introduction of swirling in the flow created a central recirculation zone in addition to the corner recirculation zone. It was found that the central recirculation zone was most prominent in the configuration with the S-inlet and swirling flow. An oscillating central core was seen in the straight inlet case. The average turbulence level was higher in the configuration with the s-inlet.

Degree

thesis:*
Name thesis:degree_name
M. S.
Level thesis:degree_level
masters
Discipline thesis:degree_discipline
Aerospace and Ocean Engineering
Department dc:contributor.department
Aerospace and Ocean Engineering
Grantor dc:publisher
Virginia Polytechnic Institute and State University
Year dc:date.issued
1983

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Guruswamy, Jayaram

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10919/114601
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/114601

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
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related terms
citation

Guruswamy, Jayaram. Effect of inlet configurations on the aerodynamics of swirl combustors. masters thesis, Virginia Polytechnic Institute and State University, 1983. http://hdl.handle.net/10919/114601