id	author	title	date	pages	extension	mime	words	sentences	flesch	summary	cache	txt
work_ofmoubrcrjdlrgegtblcgq76ru	Haifa El-sadi	Application of Computational Tools to Analyze and Test Mini Gas Turbine	2017	10	.pdf	application/pdf	2560	216	63	through a LabVIEW program running on a new laptop designated and mounted to the mini jet turbine result, The Inlet Mass Flow Rate numeric indicator value is calculated, not measured. Keywords: LabVIEW, Engineering Equation solver (EES), Mini-turbine, Pressure Gas turbine engines include internal passages which serve to channel the cooling air from compressors addition, there are sensors on this engine to monitor thrust, RPM, and fuel flow rate. Figure 2 below shows the location of each temperature and pressure being measured on the engine. In order to calculate the Inlet Mass Flow Rate to the turbine engine, the static pressure is needed. Figure.9 Engine Testing Data Plot – Thrust vs RPM engine RPM and Thrust, Temperature, Inlet Mass Flow Rate, and Pressure. Figure.8 Engine Testing Data Plot – Inlet Mass Flow Rate vs RPM These tasks and subFigure.11 Engine Testing Data Plot – Pressure vs RPM Figure.10 Engine Testing Data Plot – Temperature vs RPM	./cache/work_ofmoubrcrjdlrgegtblcgq76ru.pdf	./txt/work_ofmoubrcrjdlrgegtblcgq76ru.txt