Investigating the effect of turbine inlet temperature on the exergetic improvement potential of a small turbojet engine

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Date
2017
Author
Turan, O.
Hepbasli, A.
Karakoc, T.H.
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Abstract
This paper analyzes and evaluates exergetic improvement rate (IPex) of the components of a small turbojet engine with various turbine inlet temperatures. The engine consists of an inlet, starter generator, a centrifugal compressor, a reverse flow combusti
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https://www.scopus.com/inward/record.uri?eid=2-s2.0-85032380071&doi=10.1109%2fICMAE.2017.8038660&partnerID=40&md5=5905ec92459281eb9efb70fcab7d3570
https://dspace.yasar.edu.tr/xmlui/handle/20.500.12742/10054
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