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Structural optimization of composite panels under strength and stability restrictions

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Strength of Materials Aims and scope

The paper addresses a problem of optimization of structure of a composite material for smooth panels under strength and stability restrictions. Types of optimal structures have been substantiated. A series of numerical experiments have been carried out to verify the conclusions stated.

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References

  1. Ya. S. Karpov, “Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions,” Strength Mater., 36, No. 6, 570–581 (2004).

    Article  CAS  Google Scholar 

  2. Ya. S. Karpov, P. M. Gagauz, and F. M. Gagauz, “Optimal design of composite material structure for aircraft wing skin panels,” in: Open IT and Computer-Integrated Technologies [in Russian], Collected Papers, Kharkov (2003), Issue 16, pp. 40–44.

  3. Ya. S. Karpov, “Solving the fundamental problem of design of the composite material structure,” in: Issues of Design and Manufacture of Aircraft Structures [in Russian], Collected Papers, Kharkov Aviation Institute, Kharkov (2001), Issue 27, pp. 18–25.

  4. A. S. Vol’mir, Stability of Deformable Systems [in Russian], Nauka, Moscow (1967).

    Google Scholar 

  5. V. V. Vasil’ev, Mechanics of Structures of Composite Materials [in Russian], Mashinostroenie, Moscow (1988).

    Google Scholar 

  6. S. G. Lekhnitskii, Anisotropic Plates [in Russian], Gostekhizdat, Moscow (1957).

    Google Scholar 

  7. N. S. Azikov, V. V. Vasil’ev, and A. D. Paterekas, “Stability of composite panels in compression and shear,” Mekh. Kompoz. Mater., No. 2, 351–353 (1990).

  8. Material Properties, T300/934 Carbon/Epoxy, The New York Times Company, http://composite.about.com/library/data/blc-t300-934-1.htm.

  9. P. M. Gagauz, “CM structural optimization allowing for design and technological restrictions on the stack thickness,” in: Issues of Design and Manufacture of Aircraft Structures [in Russian], Collected Papers, Kharkov Aviation Institute, Kharkov (2008), Issue 2 (53), pp. 121–126.

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Authors and Affiliations

  1. Zhukovskii National Aerospace University “Kharkov Aviation Institute”, Kharkov, Ukraine

    Ya. S. Karpov & P. M. Gagauz

Authors
  1. Ya. S. Karpov
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  2. P. M. Gagauz
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Translated from Problemy Prochnosti, No. 6, pp. 5–12, November–December, 2010.

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Karpov, Y.S., Gagauz, P.M. Structural optimization of composite panels under strength and stability restrictions. Strength Mater 42, 631–636 (2010). https://doi.org/10.1007/s11223-010-9251-z

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  • DOI: https://doi.org/10.1007/s11223-010-9251-z

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