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NASA NTRS · 20030048822

A Study of Fan Stage/Casing Interaction Models

Abstract

The purpose of the present study is to investigate the performance of several existing and new, blade-case interactions modeling capabilities that are compatible with the large system simulations used to capture structural response during blade-out events. Three contact models are examined for simulating the interactions between a rotor bladed disk and a case: a radial and linear gap element and a new element based on a hydrodynamic formulation. The first two models are currently available in commercial finite element codes such as NASTRAN and have been showed to perform adequately for simulating rotor-case interactions. The hydrodynamic model, although not readily available in commercial codes, may prove to be better able to characterize rotor-case interactions.

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BibTeXRIS

Lawrence, Charles, Carney, Kelly, Gallardo, Vicente. 2003-03-01. A Study of Fan Stage/Casing Interaction Models. https://ntrs.nasa.gov/citations/20030048822

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