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Simplified design procedures for fiber composite structural components/jointsSimplified step-by-step design procedures are summarized, which are suitable for the preliminary design of composite structural components such as panels (laminates) and composite built-up structures (box beams). Similar procedures are also summarized for the preliminary design of composite bolted and adhesively bonded joints. The summary is presented in terms of sample design cases complemented with typical results. Guidelines are provided which can be used in the design selection process of composite structural components/joints. Also, procedures to account for cyclic loads, hygrothermal effects and lamination residual stresses are included.
Document ID
19900015068
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murthy, P. L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:103113
E-5392
NASA-TM-103113
Report Number: NAS 1.15:103113
Report Number: E-5392
Report Number: NASA-TM-103113
Meeting Information
Meeting: Indo-US Workshop on Composite Materials for Aerospace Applications
Location: Bangalore
Country: India
Start Date: July 23, 1990
End Date: July 27, 1990
Sponsors: Indian Inst. of Science
Accession Number
90N24384
Funding Number(s)
PROJECT: RTOP 505-63-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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