Preliminary Results of an Altitude-Wind-Tunnel Investigation of a TG-100A Gas Turbine-Propeller Engine

An investigation to determine the performance and operational characteristics of the TG-1OOA gas turbine-propeller engine was conducted in the Cleveland altitude wind tunnel. As part of this investigation, the combustion-chamber performance was determined at pressure altitudes from 5000 to 35,000 fe...

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Bibliographische Detailangaben

Hauptverfasser:	Gensenheyner, Robert M., Berdysz, Joseph J.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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