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Design Procedures for Fiber Composite Box BeamsStep-by-step procedures are described which can be used for the preliminary design of fiber composite box beams subjected to combined loadings. These procedures include a collection of approximate closed-form equations so that all the required calculations can be performed using pocket calculators. Included is an illustrated example of a tapered cantilever box beam subjected to combined loads. The box beam is designed to satisfy strength, displacement, buckling, and frequency requirements.
Document ID
19880007444
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH., United States)
Murthy, Pappu L. N.
(Cleveland State Univ. Ohio., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:100296
NASA-TM-100296
E-3296
Report Number: NAS 1.15:100296
Report Number: NASA-TM-100296
Report Number: E-3296
Accession Number
88N16828
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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