Мобильная версия

Доступно журналов:

3 288

Доступно статей:

3 891 637

 

Скрыть метаданые

Автор Whitcomb, John, D.
Автор Shivakumar, K.N.
Дата выпуска 1989
dc.description Delamination growth due to local buckling of a delamination was studied. Delamination growth was assumed to be related to the total strain-energy release rate, G. In order to calculate the distribution of G along the delamination front, a virtual crack closure technique was developed which is suitable for use with plate analysis. A check of the technique indicated that it is accurate. For square and rectangular delaminations, there is a large variation of G along the delamination front. Hence, self-similar growth is not ex pected. Whether a delamination grows in the load direction or perpendicular to the load direction was found to depend on the current delamination aspect ratio, the strain level, and the absolute size of the delamination.
Издатель Sage Publications
Название Strain-Energy Release Rate Analysis of Plates with Postbuckled Delaminations
Тип Journal Article
DOI 10.1177/002199838902300705
Print ISSN 0021-9983
Журнал Journal of Composite Materials
Том 23
Первая страница 714
Последняя страница 734
Аффилиация Whitcomb, John, D., NASA Langley Research Center Mail Stop 188E Hampton, VA 23665-5225
Аффилиация Shivakumar, K.N., Analytical Services and Materials, Inc. NASA Langley Research Center Mail Stop 188E Hampton, VA 23665-5225
Выпуск 7
Библиографическая ссылка Byers, B.A.Behavior of Damaged Graphite/Epoxy Laminates Under Compression Loading , NASA CR-159293 (August 1980).
Библиографическая ссылка Porter, T.R.Compression and Compression Fatigue Testing of Composite Laminates , NASA CR-168023 (July 1982).
Библиографическая ссылка Konishi, D.Y. and W.R. Johnson. "Fatigue Effects on Delaminations and Strength Degradation in Graphite/Epoxy Laminates," Composite Materials: Testing and Design, Fifth Conference, ASTM STP, American Society for Testing and Materials, pp. 597-619 (1979).
Библиографическая ссылка Whitcomb, J.D. "Strain-Energy Release Rate Analysis of Cyclic Delamination Growth in Compressively Loaded Laminates," Effects of Defects in Composite Materials, ASTM STP 836, American Society for Testing and Materials , Philadelphia, Pa., pp. 175-193 (1984).
Библиографическая ссылка Whitcomb, J.D. "Finite Element Analysis of Instability-Related Delamination Growth," J. Composite Materials, 15:403-426 (1981).
Библиографическая ссылка Whitcomb, J.D. "Parametric Analytical Study of Instability-Related Delamination Growth," Composites Science and Technology, 25:19-48 (1986).
Библиографическая ссылка Chai, H., C.D. Babcock and W.G. Knauss. "One Dimensional Modeling of Failure in Laminated Plates by Delamination Buckling," Int. J. of Solids Structures, 17(11):1069-1083 (1981).
Библиографическая ссылка Chai, H. and C.D. Babcock. "Two-Dimensional Modeling of Compressive Failure in Delaminated Laminates," Journal of Composite Materials, 19:67-98 (January 1985).
Библиографическая ссылка Irwin, G.R. "Analysis of Stresses and Strains Near the End of a Crack Traversing a Plate," Journal of Applied Mechanics, Transactions of ASME, pp. 361-364 (September 1957).
Библиографическая ссылка Ugural, A.C.Stresses in Plates and Shells, New York, NY: McGraw-Hill, p. 93 (1981).
Библиографическая ссылка Timoshenko, S.P. and S. Woinowski-Krieger . Theory of Plates and Shells, New York, NY:McGraw-Hill, pp. 203-206 (1959).
Библиографическая ссылка Almroth, B.O., F.A. Brogan and G.M. Stanley. Structural Analysis of General Shells, Vol. 2, User Instructions for STAGSC-1. Lockheed Palo Alto Research Laboratory, Palo Alto, CA (1982).

Скрыть метаданые