Linearized blade row compression component model. Stability and frequency response analysis of a J85-3 compressor

NASA developed stability and frequency response analysis techniques were applied to a dynamic blade row compression component stability model to provide a more economic approach to surge line and frequency response determination than that provided by time-dependent methods. This blade row model was...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Tesch, W. A., Moszee, R. H., Steenken, W. G.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!