Performance of Compressor of XJ-41-V Turbojet Engine II - Static-Pressure Ratios and Limitation of Maximum Flow at Equivalent Compressor Speed of 8000 rpm

At the request of the Air Material Command, Army Air Forces, an investigation was conducted by the NACA Cleveland laboratory to determine the performance characteristics of the compressor of the XJ-41-V turbojet engine. This report is the second in a series presenting the compressor performance and...

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Bibliographische Detailangaben

Hauptverfasser:	Dildine, Dean M., Arthur, W. Lewis
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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