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Автор Gruber, Mark, B.
Автор Lamontia, Mark, A.
Автор Smoot, Michael, A.
Автор Peros, Vasilios
Дата выпуска 1995
dc.description The general instability, or buckling performance, of thick compression loaded composite cylinders is not well understood. Few cylinders have been hydrostatically tested that exhibit a well-controlled buckling failure. This work includes the design, fabrication, and test results for two monocoque cylinders tested in hydrostatic compression to measure buckling performance. The design focused on assuring that buckling failure would occur before a strength failure. The analysis accounted for the effects of end cap design and boundary conditions. The two cylinders were insitu thermoplastic filament wound using AS4 Graphite/PEKK and S-2 Glass/PEKK. Quality was excellent, with 1% void volume fraction and negligible waviness. Both cylinders buckled elastically in their respective tests. The test results include acoustic emissions (AE) and measured strains versus pressure. Experimental results show excellent correlation with analytical predictions.
Издатель TECHNOMIC PUBLISHING CO., INC.
Название Buckling Performance of Hydrostatic Compression-Loaded 7-Inch Diameter Thermoplastic Composite Monocoque Cylinders
Тип Journal Article
DOI 10.1177/089270579500800107
Print ISSN 0892-7057
Журнал Journal of Thermoplastic Composite Materials
Том 8
Первая страница 94
Последняя страница 108
Аффилиация Smoot, Michael, A., Du Pont Advanced Material Systems, Delaware Technology Park, P0. Box 6108, Newark, DE 19714-6108
Аффилиация Peros, Vasilios, Martin Marietta Aero & Naval Systems, Baltimore, MD 21220
Выпуск 1
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Библиографическая ссылка 2. Roberts, B. K., M. A. Lamontia, M. B. Gruber, K. B. Su, K. L. Adams, T. W. Harding, M. A. Smoot and D. R. Root. 1991. "Advanced Submarine Technology Thermoplastic Materials Program, Phase HA, Final Report" DARPA, ARPA Order No. 6661; Program Code No. 6661/22/23.
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Библиографическая ссылка 7. Martin Marietta Aero and Naval Systems, "Cylinder Computer Program-Theory of Elasticity Solution;" Final Report to the Du Pont Company, December 6, 1989.
Библиографическая ссылка 8. Miller, R. J.1969. "End Plugs for External Pressure Tests of Composite Cylinders,"Composite Material: Testing and Design, ASIM STP 460American Society for Testing and Materials, pp. 150-159.
Библиографическая ссылка 9. Bushnell, D."BOSOR4-Program for Stress, Stability, and Vibration of Complex, Branched Shells of Revolution,"Lockheed Missiles & Space Company, Inc.
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