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タイトルDesign, ancillary testing, analysis and fabrication data for the advanced composite stabilizer for Boeing 737 aircraft, volume 2
本文(外部サイト)http://hdl.handle.net/2060/19850005605
著者(英)Mccarty, J. E.; Wogulis, E. R.; Peterson, D. C.; Pritchett, L. D.; Harvey, S. T.; Aniversario, R. B.; Wilson, D. R.; Parsons, J. T.
著者所属(英)Boeing Commercial Airplane Co.
発行日1982-12-01
言語eng
内容記述Results of tests conducted to demonstrate that composite structures save weight, possess long term durability, and can be fabricated at costs competitive with conventional metal structures are presented with focus on the use of graphite-epoxy in the design of a stabilizer for the Boeing 737 aircraft. Component definition, materials evaluation, material design properties, and structural elements tests are discussed. Fabrication development, as well as structural repair and inspection are also examined.
NASA分類COMPOSITE MATERIALS
レポートNO85N13914
D6-46037-2-VOL-2
NASA-CR-166011
NAS 1.26:166011
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/157667


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