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Application of boron/epoxy reinforced aluminum stringers for the CH-54B helicopter tail cone. Phase 1: Design, analysis, fabrication and testDesign, fabrication and tests of boron/epoxy reinforced stringers for CH-54B tail cone
Document ID
19710024537
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Welge, R. T. (United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-CR-111929
Report Number: NASA-CR-111929
Accession Number
71N34013
Funding Number(s)
CONTRACT_GRANT: NAS1-10459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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