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A Mixed Finite Analysis of Axial ForeshorteningIn previous studies, a mixed finite element was derived and shown to be effective in facilitating accurate modal reduction of rotor blades. This study builds upon that earlier work through the development of algorithms that allow the element's Lagrangian axial displacement degrees of freedom to be eliminated in favor of the axial force degrees of freedom. This reduction process, which had been demonstrated previously for the case of a single mixed finite element, may be viewed as a generalization of the UMARC blade analysis methodology to arbitrary topologies. A unique strength of the method. developed here is that the model may consist of two dimensional or even three dimensional elements.
Document ID
20010062808
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Ruzicka, Gene
(NASA Ames Research Center Moffett Field, CA United States)
Rutkowski, Michael
Date Acquired
August 20, 2013
Publication Date
January 1, 2000
Subject Category
Aerodynamics
Meeting Information
Meeting: AHS Aeromechanics Specialists'' Meeting
Country: Unknown
Start Date: November 13, 2000
End Date: November 15, 2000
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
PROJECT: RTOP 712-10-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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