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Stiffness and strength tailoring in uniform space-filling truss structuresA deterministic procedure for tailoring the continuum stiffness and strength of uniform space-filling truss structures, through the appropriate selection of truss geometry and member sizes (flexural stiffness, axial stiffness, and length), is presented. The trusses considered herein are generated by uniform replication of a characteristic truss cell. The repeating cells are categorized by one of a set of possible geometric symmetry groups derived using crystallographic techniques. The elastic symmetry associated with each geometric symmetry group is identified to help select an appropriate truss geometry for a given application. Stiffness and strength tailoring of a given truss geometry is enabled through explicit expressions relating the continuum stiffnesses and failure stresses of the truss to the stiffnesses and failure loads of its members. These expressions are derived using an existing equivalent continuum analysis technique and a newly developed analytical failure theory for trusses. Several examples are presented to illustrate the application of these techniques and to demonstrate the usefulness of the information gained from this analysis.
Document ID
19920015303
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lake, Mark S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TP-3210
NAS 1.60:3210
L-17001
Report Number: NASA-TP-3210
Report Number: NAS 1.60:3210
Report Number: L-17001
Meeting Information
Meeting: DOD/NASA/FAA Conference on Fibrous Composites in Structural Design
Location: Lake Tahoe, NV
Country: United States
Start Date: November 4, 1991
End Date: November 7, 1991
Accession Number
92N24546
Funding Number(s)
PROJECT: RTOP 506-43-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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