Micro gas turbine performance evaluation

dc.contributor.authorOppong, F.
dc.contributor.authorVan Der Spuy, S.J
dc.contributor.authorVon Backstrȯm, T.W.
dc.contributor.authorLacina Diaby, A.
dc.date.accessioned2023-09-11T11:38:43Z
dc.date.available2023-09-11T11:38:43Z
dc.date.issued2017
dc.description.abstractThe deployment of Micro Gas Turbine (MGT) engines in unmanned aerial vehicles, hybrid electric vehicles, and small power plant applications is increasingly becoming popular due to their high power to weight ratios. In this paper, MGT performance evaluation is investigated for the Baird Micro Turbine 120 Kerosene Start engine (BMT 120 KS). This investigation involves component matching of the engine and its modifications. Analytical and numerical approaches were employed to review the thermodynamic cycle of the engine. The performance predictions of the engine and its modifications were found to correlate well with available engine experimental dataen_US
dc.identifier.urihttp://localhost:8080/xmlui/handle/123456789/793
dc.language.isoenen_US
dc.publisherUniversity of Mines and Technologyen_US
dc.subjectSimulationen_US
dc.subjectGasTurben_US
dc.subjectFlownexen_US
dc.subjectComponent Matchingen_US
dc.titleMicro gas turbine performance evaluationen_US
dc.typeArticleen_US

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