Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
FATIGUE AND RESIDUAL STRENGTH TESTS OF THE FULL-SCALE COMPOSITE WING BOX OF A PASSENGER AIRCRAFT
RÉSUMÉ
For the first time, fatigue and residual strength tests were performed on the wing box, which was manufactured using a polymer composite material according to a new infusion technology. The effect of technological (porosity, delamination, etc.) and operational (impact) defects on the durability and residual strength of the structure is evaluated.
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O'Brien, T.K., Towards a Damage Tolerance Philosophy for Composite Materials and Structures, NASA Technical Memorandum 100548, National Aeronautics and Space Administration, Langley Research Center, Hampton, VA, 1988.
-
Tay, T.E., Characterization and Analysis of Delamination Fracture in Composites: An Overview of Developments from 1990 to 2001, Appl. Mech. Rev, 56(1):1-32, 2003.
-
Pagano, N.J. and Schoeppner, G.A., Delamination of Polymer Matrix Composites: Problems and Assessment, in Comprehensive Composite Materials, Oxford, U.K.: Elsevier Science, pp. 1-96,2000.
-
Mitryaykin, V.I., Nedel'ko, D.V., Saltykov, S.V., and Shuvalov, V.A., Application of the Finite Element Method for Investigation of Influence of Technological Damage on Strength Characteristics of Layered Composite Structures, TsAGISci. J, 49(8):903-912, 2018.
-
Composite Materials Handbook 17 Organization (CMH-17), Ed., Composite Materials Handbook: Volume 3-Polymer Matrix Composites: Materials Usage, Design and Analysis, Warrendale, PA: SAE International, 2012.
-
Harris, B., Ed., Fatigue in Composites: Science and Technology of the Fatigue Response of Fibre-Reinforced Plastics, Cambridge, U.K.: Woodhead Publishing, 2003.
-
Shcherban K. S., Surnachev A. A., Naumov S. M., Sterlin A. Ya., Kalish A. G., Chuvilin O. V., Static and fatigue testing using the same full-scale transport aircraft structure, Industrial laboratory. Diagnostics of materials, 86, 12, 2020. Crossref