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Finite element analysis of helicopter structuresApplication of the finite element analysis is now being expanded to three dimensional analysis of mechanical components. Examples are presented for airframe, mechanical components, and composite structure calculations. Data are detailed on the increase of model size, computer usage, and the effect on reducing stress analysis costs. Future applications for use of finite element analysis for helicopter structures are projected.
Document ID
19790002282
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rich, M. J.
(Sikorsky Aircraft Stratford, CT, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Res. in Computerized Structural Analysis and Syn.,
Subject Category
Structural Mechanics
Accession Number
79N10453
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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