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Stability and dynamic analysis of a slender column with curved longitudinal stiffenersThe results of a stability design study are presented for a slender column with curved longitudinal stiffeners for large space structure applications. Linear stability analyses are performed using a link-plate representation of the stiffeners to determine stiffener local buckling stresses. Results from a set of parametric analyses are used to determine an approximate explicit expression for stiffener local buckling in terms of its geometric parameters. This expression along with other equations governing column stability and mass are assembled into a determinate system describing minimum mass stiffened column design. An iterative solution is determined to solve this system and a computer program incorporating this routine is presented. Example design problems are presented which verify the solution accuracy and illustrate the implementation of the solution routine. Also, observations are made which lead to a greatly simplified first iteration design equation relating the percent increase in column mass to the percent increase in column buckling load. From this, generalizations are drawn as to the mass savings offered by the stiffened column concept. Finally, the percent increase in fundamental column vibration frequency due to the addition of deployable stiffeners is studied.
Document ID
19890017844
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lake, Mark S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:101636
NASA-TM-101636
Report Number: NAS 1.15:101636
Report Number: NASA-TM-101636
Accession Number
89N27215
Funding Number(s)
PROJECT: RTOP 506-43-31-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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