Micro gas turbine performance evaluation

Oppong, F.; Van Der Spuy, S.J; Von Backstrȯm, T.W.; Lacina Diaby, A.

dc.contributor.author	Oppong, F.
dc.contributor.author	Van Der Spuy, S.J
dc.contributor.author	Von Backstrȯm, T.W.
dc.contributor.author	Lacina Diaby, A.
dc.date.accessioned	2023-09-11T11:38:43Z
dc.date.available	2023-09-11T11:38:43Z
dc.date.issued	2017
dc.identifier.uri	http://localhost:8080/xmlui/handle/123456789/793
dc.description.abstract	The 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 data	en_US
dc.language.iso	en	en_US
dc.publisher	University of Mines and Technology	en_US
dc.subject	Simulation	en_US
dc.subject	GasTurb	en_US
dc.subject	Flownex	en_US
dc.subject	Component Matching	en_US
dc.title	Micro gas turbine performance evaluation	en_US
dc.type	Article	en_US