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JOURNALS // Zhurnal Srednevolzhskogo Matematicheskogo Obshchestva

Zhurnal SVMO, 2019, Volume 21, Number 3, Pages 343–352 (Mi svmo747)

Strength analysis of composite rotor helicopter blade, having percussive damage, by limit equilibrium theory
I. N. Sidorov, V. I. Mitryaikin, A. V. Gorelov, L. P. Shabalin

References

1. A. V. Gorelov, I. N. Sidorov, “A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. The basic steps of an algorithm”, Russian Aeronautics, 54:3 (2011), 233–241  crossref  elib
2. A. V. Gorelov, I. N. Sidorov, “A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. Analysis results”, Russian Aeronautics, 54:4 (2011), 341–345  crossref  elib
3. R. A. Kayumov, “The method of variation of elastic characteristics in the ultimate load problem”, Prikladnaja mehanika i tehnicheskaja fizika, 1990, no. 3, 134–139 (In Russ)
4. R. A. Kayumov, “A method for two-sided limiting load estimation”, Strength of Materials, 24:1 (1992), 64–70  crossref
5. R. A. Kayumov, “On the assessment of the bearing capacity of structures under arbitrary flow conditions”, Prikladnaja mehanika i tehnicheskaja fizika, 1993, no. 1, 115–120 (In Russ)  zmath
6. I. G. Teregulov, R. A. Kajumov, Je. S. Sibgatullin, Structural analysis according to the theory of limit equilibrium, FJeN, Kazan, 2003, 180 pp. (In Russ)
7. O. O. Dunai, Y. A. Denisov, I. N. Sidorov, “Experimental study of damping properties of a composite torsion bar in the helicopter main rotor hingeless hub”, Russian Aeronautics, 52:3 (2009), 259–263  crossref  elib
8. K. E. Sibgatullin, E. S. Sibgatullin, “Estimate of strength of anisotropic bars of arbitrary cross-section in the general case of their combined stress”, Mechanics of Solids, 45:1 (2010), 67–73  crossref  adsnasa
9. A. A. Gvozdev, Calculation of the bearing capacity of structures by the method of limit equilibrium, Strojizdat, M., 1949, 280 pp. (In Russ)
10. A. V. Gorelov, I. N. Sidorov, Calculation of the stress-strain and ultimate state of the rotor composite blade of the ANSAT helicopter, Dep. in VINITI 17.07.2006, 946–B2006, Kazan, 2006, 40 pp. (In Russ)
11. V. I. Mitrjajkin, N. V. Pavlova, A. D. Lustin, “Diagnosis of impact damage to helicopter blades on a computer tomograph”, Innovacionnye podhody v sovremennoj nauke, 2017, no. 2(2), 33–40 (In Russ)
12. V. I. Mitrjajkin, T. A. Zajceva, E. V. Krotova, “Diagnostics of the state of composite structural elements on a spiral computed tomograph”, Problemy teplomassoobmena i gidrodinamiki v jenergomashinostroenii: Materialy dokladov X shkoly-seminara molodyh uchenyh i specialistov akademika RAN V. E. Alemasova (Kazan, 13 – 15 September 2016), 2016, 272–273 (In Russ)  mathscinet


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