Skip to main content
SpringerLink
Log in

Special features in ensuring strength and service life of aircraft structures made of polymer composite materials, with damage taken into account

  • Published:
Mechanics of Composite Materials Aims and scope

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Literature cited

  1. A. E. Ushakov and V. A. Kireev, “Determination of the load-bearing capacity of compressed carbon-plastic shells with and without stress raisers at elevated temperature,” Mekh. Kompozitn. Mater., No. 2, 299–305 (1988).

    Google Scholar 

  2. A. F. Selikhov, “Ensuring the service life of structures (experience in aircraft construction),” Mashinovedenie, No. 5, 11–18 (1986).

    Google Scholar 

  3. Standards of Airworthiness of Civilian Aircraft of the USSR, 3rd edn. [in Russian], Moscow (1979).

  4. A. F. Selikhov, V. L. Raikher, and I. G. Khlebnikova, “Multiplicity of critical places of structures taken into account in the evaluation of endurance and service life,” Uch. Zap. TsAGI,15, No. 2, 72–81 (1984).

    Google Scholar 

  5. G. Lubin and S. J. Dastin, “Aerospace application of composites,” in: Handbook of Composites (1982), pp. 722–743.

  6. Yu. P. Trunin, A. E. Ushakov, G. B. Shalun, and N. G. Faizrakhmanov, “Experimental investigation of methods of ensuring operational service life of carbon-plastic structures in uniaxial tension,” Mekh. Kompozitn. Mater., No. 5, 931–933 (1986).

    Google Scholar 

  7. A. E. Ushakov and T. G. Podlipnaya, “Experimental investigation of the strength of carbon-plastic panels with crack stoppers having designed notches,” Mekh. Kompozitn. Mater., No. 3, 493–498 (1987).

    Google Scholar 

  8. A. E. Ushakov, I. P. Bareishis, and V. V. Paulauskas, “Characteristics of the operational service life of the glider LAK-12 ‘Letuva’ made of composite materials, at the stage of certification,” Mekh. Kompozitn. Mater., No. 5, 878–883 (1989).

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. N. E. Zhukovskii Central Institute of Aerohydrodynamics, Moscow

    A. F. Selikhov, V. F. Kut'ynov & A. E. Ushakov

Authors
  1. A. F. Selikhov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. V. F. Kut'ynov
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. A. E. Ushakov
    View author publications

    You can also search for this author in PubMed Google Scholar

Additional information

Translated from Mekhanika Kompozitnykh Materialov, No. 3, pp. 469–479, May–June, 1990.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Selikhov, A.F., Kut'ynov, V.F. & Ushakov, A.E. Special features in ensuring strength and service life of aircraft structures made of polymer composite materials, with damage taken into account. Mech Compos Mater 26, 349–357 (1990). https://doi.org/10.1007/BF00613113

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF00613113

Keywords

Search

Navigation