Aircraft air intakes location impact on vortex formation intensity

Аuthors

Panov S. Y., Kovalev A. V., Aisin A. K.^*, Achekin A. A.

Air force academy named after professor N.E. Zhukovskii and Y.A. Gagarin, Voronezh, Russia

*e-mail: aisin_alex@mail.ru

Abstract

Keywords:

experimental studies, vortex, vortex formation intensity, air intake, gas-turbine engine, protection method, foreign objects ingress

References

1. Evdokimov A.I., Neskoromnyi E.V., Markov D.S. Nasosy. Turbiny. Sistemy, 2017, no. 4(25), pp. 35–42.

2. Leont’ev M.K., Berne A.L. Vestnik Moskovskogo aviatsionnogo instituta, 1998, vol. 5, no. 2, pp. 26-32.

3. Fulton G.B. Design and qualification of foreign object damage resistant turbofan blades. AIAA/SAE 11th Propulsion Conference, Anaheim, September 1975. Paper № 75-1313.

4. Golubev V.A., Kotovich A.V. Vestnik Moskovskogo Aviatsionnogo instituta, 1994, vol. 1, no. 1, pp. 20-27.

5. Ryabov A.A., Romanov V.I., Kukanov S.S., Shmotin Yu.N., Chupin P.V. Vestnik Moskovskogo aviatsionnogo instituta, 2011, vol. 18, no. 3, pp. 266-273.

6. Besedov N.P. Uchenye zapiski TsAGI, 1975, vol. 6, no. 3, pp. 99-104.

7. Biksaev A.Sh., Senyushkin N.S., Kalimullin R.R., Belobrovina M.V. Materialy II Mezhdunarodnoi nauchnoi konferentsii “Tekhnicheskie nauki: traditsii i innovatsii” (Chelyabinsk, October 2013, Chelyabinsk, Dva komsomol’tsa, 2013, pp. 54-56. URL: https://moluch.ru/conf/tech/archive/87/4187/

8. Komov A.A., Yurin S.P. Nauchnyi vestnik GosNIIGA, 2014, no. 4, pp. 42-48.

9. Komov A.A. Teoreticheskie osnovy i tekhnicheskie resheniya dlya zashchity aviatsionnykh dvigatelei ot popadaniya tverdykh postoronnikh predmetov s poverkhnosti aerodrome (Theoretical foundations and technical solutions for aircraft engines protection from foreign solid objects ingress from the airfield surface). Doctor’s thesis, Moscow, GosNIIGA, 2005, 400 p.

10. Komov A.A. Materialy XII Vserossiiskoi nauchno-tekhnicheskoi konferentsii “Nauchnye chteniya po aviatsii, posvyashchennye pamyati N.E. Zhukovskogo”, Moscow, Izdatel’skii dom Akademii imeni N.E. Zhukovskogo, 2015, pp. 132-133.

11. Pakhomov S.V., Safarbakov A.M. Metody i sredstva zashchity gazoturbinnykh dvigatelei vozdushnykh sudov ot popadaniya postoronnikh predmetov (Methods and means of aircraft gas turbine engines protection from foreign objects ingress), Irkutsk, IrGUPS, 2011. Part 2, 156 p.

12. Colehour J.L., Farquhar B.W. Inlet Vortex. Journal of Aircraft, 1971, vol. 8, no. 1, pp. 39-43. DOI: 10.2514/3.44224

13. Cernoch L., Kachler H.B. Damage-tolerant fan blade design. AIAA Paper № 79-1119.

14. Kizim V.Ya., Komov A.A. Materialy Vsesoyuznoi nauchno-tekhnicheskoi konferentsii “Problema zashchity GTD ot povrezhdenii postoronnimi predmetami”, Zhukovskii, LII im. M.M. Gromova, 1978, pp. 32-33.

15. Komov A.A. Konstruktsiya i sistemy upravleniya GTD. Sbornik statei, Moscow, VVIA im. prof. N.E. Zhukovskogo, 2001, pp. 35-49.

16. Komov A.A. Nauchnyi vestnik MGTUGA, 2005, no. 90, pp. 123-128.

17. Slobodkina F.A., Malinin V.V. Dvigatel’, 2009, no. 3(63), pp. 4-7.

18. Launder B.E. and Spalding D.B. B. The Numerical Computation of Turbulent Flows. Computer Methods in Applied Mechanics and Engineering. 1974, vol. 3, issue 2, pp. 269-289. DOI: 10.1016/0045-7825(74)90029-2

19. Komov A.A., Evdokimov A.I. Mezhdunarodnyi aviatsionno-kosmicheskii salon (Zhukovskii, 14-19 August 2001). Sbornik statei. Moscow, RA Intervestnik, 2001, pp. 85-89.

20. Slobodkina F.A., Malinin V.V. Aviatsionno-kosmicheskaya tekhnika i tekhnologiya. 2006. № 10(36).