@thesis{thesis,
		author={FIRDANI  ANGGI},
		title ={ANALISIS EFISIENSI OVERALL TURBOPROP ENGINE
GARRETT TPE331-10R-512C PESAWAT CASA 212},
		year={2018},
		url={http://eprints.stta.ac.id/2366/},
		abstract={A Garrett TPE331 engine that has been serviced,
is first tested to determine the performance of the engine. The purpose of this thesis is to determine the overall efficiency of the Garrett TPE331 engine of the CASA 212 aircraft using Parametric Cycle Analysis of Real Engine.
The method used is a calculation method whose calculations use the "Mathcad" software. To start the calculation, several input data parameters are needed that have been obtained from references and Garrett TPE331 engine test data. These parameters are used to determine the overall efficiency of the TPE331 turboprop engine.
In calculating overall efficiency, the parameters used in the calculation are the propulsive efficiency and thermal efficiency values ??obtained from the calculation results using the equations in Jack D Matingly's book. The overall efficiency value at Mach Number 0.282 is 8.2%, at Mach Number 0.678 it is 29.8%.}
		}