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dc.contributor.authorWadey, Alexanderen
dc.description.abstractEvaporative spray cooling is a technique that utilizes the latent heat of evaporation of a cold liquid spray to rapidly cool a hot gaseous source. During evaporation the liquid droplets are fixed at their boiling point, ensuring a large temperature differential between liquid and gas, and promoting high heat transfer rates. The application of note for this research is the infrared radiation (IR) suppression of naval vessel exhaust streams which have a distinctive radiative signature due to the hot carbon dioxide and water vapour within the exhaust. Cooling of the exhaust stream greatly reduces this signature and limits the possibility of tracking by hostile sources [1]. Despite extensive and historical use in fields such as fire suppression, the detailed mechanics of evaporative sprays are incredibly complex and predictive simulation of these flows has only been made possible with the rapid increase in computational power over the last two decades [2]. This research presents a dual approach in which results from optical measurements of a scale naval vessel exhaust system equipped with evaporative spray cooling are compared with the findings of multi-phase spray flow computational fluid dynamics (CFD). Spray flow experiments were run at the Grant Timmins research facility on the Hot Gas Wind Tunnel (HGWT), a rig capable of emulating a scale naval vessel exhaust system. With previous research focussing on direct spray measurement, an optical approach was undertaken utilizing a laser sheet to produce overall spray images and high-speed droplet imagery. In conjunction with experimentation a spray flow CFD study was constructed within the ANSYS suite of software tools. Given the complexity of real-world spray mechanics, simplified models form the bulk of the droplet-gas interaction within CFD and ensuring these models perform well together forms the crux of these simulations. The CFD results produced compare well with droplet velocity measurements, but spray spread and evaporation rates do not match experiment. Despite this, it is likely that a robust predictive CFD methodology may yet be created in the same software suite given further inquiry.en
dc.relation.ispartofseriesCanadian thesesen
dc.rightsQueen's University's Thesis/Dissertation Non-Exclusive License for Deposit to QSpace and Library and Archives Canadaen
dc.rightsProQuest PhD and Master's Theses International Dissemination Agreementen
dc.rightsIntellectual Property Guidelines at Queen's Universityen
dc.rightsCopying and Preserving Your Thesisen
dc.rightsThis publication is made available by the authority of the copyright owner solely for the purpose of private study and research and may not be copied or reproduced except as permitted by the copyright laws without written authority from the copyright owner.en
dc.rightsCC0 1.0 Universal*
dc.subjectEvaporative Spray Coolingen
dc.subjectIR Suppressionen
dc.titleEvaporative Spray Cooling of Hot Air Flow from a Round Nozzle: Experiments and CFDen
dc.contributor.supervisorBirk, A.M.
dc.contributor.departmentMechanical and Materials Engineeringen's University at Kingstonen

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Queen's University's Thesis/Dissertation Non-Exclusive License for Deposit to QSpace and Library and Archives Canada
Except where otherwise noted, this item's license is described as Queen's University's Thesis/Dissertation Non-Exclusive License for Deposit to QSpace and Library and Archives Canada