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A Study of Fan Stage/Casing Interaction ModelsThe 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.
Document ID
20030048822
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Lawrence, Charles
(NASA Glenn Research Center Cleveland, OH, United States)
Carney, Kelly
(NASA Glenn Research Center Cleveland, OH, United States)
Gallardo, Vicente
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:212215
NASA/TM-2003-212215
E-13836
Report Number: NAS 1.15:212215
Report Number: NASA/TM-2003-212215
Report Number: E-13836
Funding Number(s)
WBS: WBS 22-728-30-07
Distribution Limits
Public
Copyright
Public Use Permitted.
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