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The Study of Stability of Compression-Loaded Multispan Composite Panel Upon Failure of Elements Binding it to Panel SupportsThe present document is a final technical report carried out within co-operation between United States'NASA Langley RC and Russia's Goskomoboronprom in aeronautics, and continues similar programs, accomplished in 1996, 1997, and 1998, respectively). The report provides results of "The study of stability of compression-loaded multispan composite panels upon failure of elements binding it to panel supports"; these comply with requirements established at TsAGI on 24 March 1998 and at NASA on 15 September 1998.
Document ID
20020080818
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Zamula, G. N. (Tsentralni Aerogidrodinamicheskii Inst. Zhukovsky, Russia)
Ierusalimsky, K. M. (Tsentralni Aerogidrodinamicheskii Inst. Zhukovsky, Russia)
Fomin, V. P. (Tsentralni Aerogidrodinamicheskii Inst. Zhukovsky, Russia)
Grishin, V. I. (Tsentralni Aerogidrodinamicheskii Inst. Zhukovsky, Russia)
Kalmykova, G. S. (Tsentralni Aerogidrodinamicheskii Inst. Zhukovsky, Russia)
Date Acquired
August 20, 2013
Publication Date
January 1, 1999
Subject Category
Mechanical Engineering
Funding Number(s)
CONTRACT_GRANT: NCC1-233
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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