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Selected NASA research in composite Materials and structuresVarious aspects of the application of composite materials to aircraft structures are considered. Failure prediction techniques, buckling and postbuckling research, laminate fatigue analysis, damage tolerance, high temperature resin matrix composites and electrical hazards of carbon fiber composites are among the topics discussed.
Document ID
19800019935
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Composite Materials
Report/Patent Number
L-13915
NASA-CP-2142
Report Number: L-13915
Report Number: NASA-CP-2142
Meeting Information
Meeting: Ind. Rev. of the NASA Aircraft Energy Efficiency (ACEE) Composite Programs
Location: Seattle
Start Date: August 11, 1980
End Date: August 13, 1980
Accession Number
80N28436
Funding Number(s)
PROJECT: RTOP 534-03-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19800019936WorkFailure prediction techniques for compression loaded composite laminates with holes19800019937WorkBuckling and postbuckling research on flat and curved composite panels19800019938WorkDevelopment of a laminate fatigue analysis19800019939WorkDamage tolerance research on composite compression panels19800019941WorkAn investigation of possible electrical hazards of carbon fiber composites19800019940WorkHigh Temperature Resin Matrix Composites for Aerospace Structures19800019936WorkFailure prediction techniques for compression loaded composite laminates with holes19800019937WorkBuckling and postbuckling research on flat and curved composite panels19800019938WorkDevelopment of a laminate fatigue analysis19800019939WorkDamage tolerance research on composite compression panels19800019940WorkHigh Temperature Resin Matrix Composites for Aerospace Structures19800019941WorkAn investigation of possible electrical hazards of carbon fiber composites
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