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Engine environmental effects on composite behaviorA series of programs were conducted to investigate and develop the application of composite materials to turbojet engines. A significant part of that effort was directed to establishing the impact resistance and defect growth chracteristics of composite materials over the wide range of environmental conditions found in commercial turbojet engine operations. Both analytical and empirical efforts were involved. The experimental programs and the analytical methodology development as well as an evaluation program for the use of composite materials as fan exit guide vanes are summarized.
Document ID
19800014881
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Smith, G. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-81508
E-446
Report Number: NASA-TM-81508
Report Number: E-446
Meeting Information
Meeting: Struct., Structural Dyn. and Mater. Conf.
Location: Seattle
Start Date: May 12, 1980
End Date: May 14, 1980
Sponsors: ASME, AIAA, AHS, ASCE
Accession Number
80N23370
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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