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dc.contributor.advisorSathe, Sanjeev B.
dc.contributor.advisorMillsaps, Knox T.
dc.contributor.authorKoh, Chuan Heng Erik
dc.dateSep-14
dc.date.accessioned2014-12-05T20:10:27Z
dc.date.available2014-12-05T20:10:27Z
dc.date.issued2014-09
dc.identifier.urihttps://hdl.handle.net/10945/43942
dc.description.abstractThis thesis presents the effect of exhaust tube length-to-diameter (L/d) ratio, jacket-to-tube diameter (D/d) ratio, coolant inlet and outlet placements, exhaust gas swirling conditions, and tube materials (steel, copper, Inconel, and ceramic) on heat recovery performance, exhaust side pressure drop, and temperature profile in the exhaust gas Waste Heat Recovery Unit (WHRU). Non-dimensional parametric studies of a selected counter-flow Water Jacket WHRU was conducted using analytical and Computational Fluid Dynamic (CFD) models. Exhaust gas Reynolds numbers between 20,000 and 400,000, representative of exhaust gas flow in the exhaust stacks of U.S.Marine Corps’ MEP803A diesel generators and the U.S.Navy's 501-K17 gas turbine generators, were used. Results indicate heat recovery increases with higher L/d, D/d, and swirling exhaust gases conditions but with a severe pressure drop penalty. Addition of a solid heat spreader at the exhaust gas inlet and the use of suitable tube materials were also found to influence temperature profiles in the WHRU and mitigate adverse temperature gradients to some extent without any additional pressure drop penalty. Optimal laterally shifted placement of coolant inlet and outlet was found to improve heat recovery by up to 19% and was very effective at mitigating adverse temperature profiles, which improves the reliability of exhaust gas WHRU.en_US
dc.description.urihttp://archive.org/details/performancendrel1094543942
dc.publisherMonterey, California: Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titlePerformance and reliability of exhaust gas waste heat recovery unitsen_US
dc.typeThesisen_US
dc.contributor.departmentMechanical and Aerospace Engineering (MAE)
dc.subject.authorwaste heat recoveryen_US
dc.subject.authorheat recovery performanceen_US
dc.subject.authorswirling flowen_US
dc.subject.authorpressure drop penaltyen_US
dc.subject.authortemperature profilesen_US
dc.subject.authorthermal stressesen_US
dc.description.serviceMilitary Expert 5, Republic of Singapore Navyen_US
etd.thesisdegree.nameMaster of Science in Mechanical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineMechanical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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