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Experimental Study on Compression Behavior of Fiber-Reinforced Resin-Based Composite Stiffened Panels in Hygrothermal Environment

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Strength of Materials Aims and scope

Fiber-reinforced resin-based composite stiffened panels are put in the hygrothermal box at 70°C and 85% RH until moisture absorption reaches balance. Then, the compression experiments on the common stiffened panels and the stiffened panels after moisture absorption are conducted to get buckling and failure loads. Test results are compared to analyze the effect of damage on the carrying capacity of the structure. The buckling load does not significantly change, but the failure load of the panels after moisture absorption is reduced by 10.2% as compared to the common panels. The failure modes are mainly composed of debonding and fracture of the stiffener, the skin cleavage and deformation of the specimen. The experimental results will offer some valuable guidelines to engineering applications of the structure.

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References

  1. C. Bisagni and R. Vescovini, “Analytical formulation for local buckling and post-buckling analysis of stiffened laminated panels,” Thin Wall. Struct., 47, No. 3, 318–334 (2009).

    Article  Google Scholar 

  2. W. Li and Q. F. Guo, “Application of carbon fiber composites to cosmonautic fields,” Chinese Optics, 4, No. 3, 201–212 (2011).

    CAS  Google Scholar 

  3. C. J. Wang and Y. F. Dai, “Application of carbon fiber composite in aerospace,” Dev. Innov. Mach. Electr. Prod., 23, No. 2, 83–89 (2010).

    Google Scholar 

  4. Y. Feng and Y. He, “Effect of hygrothermal environment on compressive performance of composite stiffened panel,” Mater. Mech. Eng., 39, No. 1, 73–76 (2015).

    CAS  Google Scholar 

  5. T. Ye and Y. Yue, “Numerical study and experiment of composite stringer on compressive property,” Fiber Reinforced Plastics/Composites, 7, 34–38 (2019).

    Google Scholar 

  6. Y. H. Gu, D. T. Zhang, and M. H. Jia, “Preparation and compressive properties of carbon fiber reinforced braided composite circular tubes,” J. Textile Res., 40, No. 7, 71–77 (2019).

    Google Scholar 

  7. F. Yang and Z. F. Yue, “Analysis and experiment of post-buckling characteristics of stiffened panel under compress load by arc-length method,” Chinese J. Appl. Mech., 32, No. 1, 119–124 (2015).

    Google Scholar 

  8. C. Kassapoglou, Design and Analysis of Composite Structure: With Applications to Aerospace Structure, Wiley (2010).

  9. A. P. G. Villani, M. V. Donadon, M. A. Arbelo, et al., “The postbuckling behavior of adhesively bonded stiffened panels,” Aerosp. Sci. Technol., 46, 30–41 (2015).

    Article  Google Scholar 

  10. J. Ndogmo, M. Mensinger, and I. Both, “Buckling behavior of stiffened plate under biaxial compression and shear,” Procedia Engineer., 156, 272–279 (2016).

    Article  Google Scholar 

  11. D. B. Singh and B. N. Singh, “Buckling analysis of three dimensional braided composite plates under uniaxial loading using inverse hyperbolic shear deformation theory,” Compos. Struct., 157, 360–365 (2016).

    Article  Google Scholar 

  12. Z. Liu and D. Jin, “Laminate optimization of a composite stiffened panel based on surrogate model,” J. Tsinghua Univ. (Science and Technology), 55, No. 7, 782–789 (2015).

    Google Scholar 

  13. P. Pevzner, H. Abramovich, and T. Weller, “Calculation of the collapse load of an axially compressed laminated composite stringer-stiffened curved panel – An engineering approach,” Compos. Struct., 83, No. 4, 341–353 (2008).

    Article  Google Scholar 

  14. M. C. Xu and C. G. Soares, “Assessment of the ultimate strength of narrow stiffened panel test specimens,” Thin Wall. Struct., 55, 11–21 (2012).

    Article  Google Scholar 

  15. R. Tiberkak, M. Bachene, S. Rechak, and B. Necib, “Damage prediction in composite plates subjected to low velocity impact,” Compos. Struct., 83, No. 1, 73–82 (2008).

    Article  Google Scholar 

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Correspondence to Y. He.

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Translated from Problemy Prochnosti, No. 4, pp. 176 – 183, July – August, 2020.

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An, T., He, Y. & Feng, Y. Experimental Study on Compression Behavior of Fiber-Reinforced Resin-Based Composite Stiffened Panels in Hygrothermal Environment. Strength Mater 52, 655–661 (2020). https://doi.org/10.1007/s11223-020-00216-4

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  • DOI: https://doi.org/10.1007/s11223-020-00216-4

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