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TsAGI Science Journal

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

Volume 50, Numéro 3, 2019, pp. 293-308
DOI: 10.1615/TsAGISciJ.2019031378
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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.

RÉFÉRENCES
  1. 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.

  2. 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.

  3. 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.

  4. 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.

  5. 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.

  6. Harris, B., Ed., Fatigue in Composites: Science and Technology of the Fatigue Response of Fibre-Reinforced Plastics, Cambridge, U.K.: Woodhead Publishing, 2003.

CITÉ PAR
  1. 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

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