Hydroxyl-Radical Planar Laser-Induced Fluorescence Imaging of Turbulent Supersonic Combustion

Flow visualisation and statistical analysis of a supersonic, turbulent reacting flow from non-intrusive hydroxyl radical (OH) planar laser-induced fluorescence (PLIF) images are presented. The OH PLIF images show instantaneous structures of turbulence in two combustor configurations at different fuel equivalence ratios in the University of Virginia Supersonic Combustion Facility (UVaSCF). Proper orthogonal decomposition (POD) and autocorrelations are performed on the OH PLIF data to extract quantitative information about turbulent fluctuations and length scale correlations. Changes in integral length scales and turbulent energy flow patterns are observed as a function of position in the combustor and fuel equivalence ratio. Dual-mode operation with supersonic and subsonic combustion is demonstrated in the facility. This work has been performed in collaboration with other non-intrusive diagnostic techniques in the UVaSCF to develop a comprehensive database for the validation of computational fluid dynamics (CFD) models.

Name thesis:degree_name

Master of Science (MSc)

Discipline thesis:degree_discipline

Mechanical and Manufacturing Engineering

Grantor dc:publisher.institution

Graduate Studies

Year dc:date.issued

2014

Author dc:creator

• McRae, Colin

Advisor dc:contributor.advisor

• Johansen, Craig

• Engineering--Aerospace

Statement dc:rights

• University of Calgary graduate students retain copyright ownership and moral rights for their thesis. You may use this material in any way that is permitted by the Copyright Act or through licensing that has been assigned to the document. For uses that are not allowable under copyright legislation or licensing, you are required to seek permission.

Language dc:language.iso

eng

DOI

http://dx.doi.org/10.11575/PRISM/26405

OAI identifier oai:identifier

oai:ucalgary.scholaris.ca:11023/1454