Performance of J33 turbojet engine with shaft-power extraction III : turbine performance

The performance of the turbine component of a J33 turbojet engine was determined over a range of turbine speeds from 8000 to 11,500 rpm.Turbine-inlet temperature was varied from the minimum required to drive the compressor to a maximum of approximately 2000 degrees R at each of several intermediate...

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Bibliographische Detailangaben

Hauptverfasser:	Huppert, M C, Nettles, J C
Format:	Report
Sprache:	eng
Online-Zugang:	Volltext bestellen
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