Assessment of reduced models for the detection of modal interaction through rotor stator contacts

Author:

Batailly Alain,Legrand Mathias,Cartraud Patrice,Pierre Christophe

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference19 articles.

1. Experimental results from controlled blade tip/shroud rubs at engine speed;Padova;Journal of Turbomachinery,2007

2. An experimental investigation of temperatures due to rubbing at the blade–seal interface in an aircraft compressor;Emery;Wear,1983

3. Analysis of a j69-t-25 engine turbine blade fracture;Park;Engineering Failure Analysis,2002

4. M. Legrand, Modèles de Prédiction de l’Interaction Rotor/Stator dans un Moteur d’Avion (Models of Rotor/Stator Interaction in Aircraft Engines), Thèse de Doctorat (PhD Thesis), École Centrale de Nantes, Nantes, France, 2005.

5. Two-dimensional modeling of an aircraft engine structural bladed disk-casing modal interaction;Legrand;Journal of Sound and Vibration,2009

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