A three-node C ̊element for analysis of laminated composite sandwich shells /
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Author / Creator: | Martin, C. Wayne. |
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Imprint: | [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989. |
Description: | 13 pages : illustrations ; 28 cm. |
Language: | English |
Series: | NASA technical memorandum ; 4125 NASA technical memorandum ; 4125. |
Subject: | |
Format: | E-Resource Microform U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7242238 |
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100 | 1 | |a Martin, C. Wayne. |0 http://id.loc.gov/authorities/names/n85351289 |1 http://viaf.org/viaf/30149106003468490525 | |
245 | 1 | 2 | |a A three-node C ̊element for analysis of laminated composite sandwich shells / |c C. Wayne Martin, S.F. Lung, and K.K. Gupta. |
264 | 1 | |a [Washington, DC] : |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; |a Springfield, VA : |b For sale by the National Technical Information Service, |c 1989. | |
300 | |a 13 pages : |b illustrations ; |c 28 cm. | ||
336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
337 | |a microform |b h |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/h | ||
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490 | 1 | |a NASA technical memorandum ; |v 4125 | |
504 | |a Includes bibliographical references (page 9). | ||
538 | |a Available via Internet from the NASA Technical Report Server web site. Address as of 7/10/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017842%5F1989017842.pdf; current access available via PURL. | ||
650 | 0 | |a Elastic plates and shells |x Mathematical models. | |
650 | 0 | |a Composite materials |x Mathematical models. | |
650 | 0 | |a Laminated materials |x Mathematical models. | |
650 | 0 | |a Sandwich construction |x Mathematical models. | |
650 | 7 | |a Computer programs. |2 nasat | |
650 | 7 | |a Laminates. |2 nasat | |
650 | 7 | |a Plates (structural members) |2 nasat | |
650 | 7 | |a Shear properties. |2 nasat | |
650 | 7 | |a Shells (structural forms) |2 nasat | |
650 | 7 | |a Structural analysis. |2 nasat | |
700 | 1 | |a Lung, S. F. | |
700 | 1 | |a Gupta, K. K. |0 http://id.loc.gov/authorities/names/n90675844 |1 http://viaf.org/viaf/51729483 | |
710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Division. |0 http://id.loc.gov/authorities/names/n78091123 |1 http://viaf.org/viaf/313078696 | |
830 | 0 | |a NASA technical memorandum ; |v 4125. | |
856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS96605 |y Government Publishing Office |
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