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Numerical determination of the gas-dynamic behavior of vane cascades with various deflection angles of the trailing edges of longitudinal ribs of an advanced gas-turbine engine thrust reverser

  • Aircraft and Rocket Engine Design and Development
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Abstract

The work comprises numerical investigation of the influence of the deflection angles of the trailing edges of longitudinal ribs on the gas-dynamic behavior of vane cascades of a thrust reverser located in the secondary flow of a bypass turbofan engine (BTFE). Verification of the numerical model was performed on the basis of experimental research.

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References

  1. Svyatogorov, A.A., Popov, K.N., and Khvostov, N.I., Ustroistva dlya otkloneniya reaktivnoi strui turboreaktivnykh dvigatelei (Systems for Deflection of the Jet Streams of Turbojet Engines), Moscow: Mashinostroenie, 1968.

    Google Scholar 

  2. Polyakov, V.V., Golubev, V.A., and Bondarev, O.V., Reversivnye ustroistva VRD (Airbreathing Engine Thrust Reversers), Moscow: MAI, 1990.

    Google Scholar 

  3. Danil’chenko, V.P., Lukachev, S.V., and Kovylov, Yu.L., Proekrirovanie aviatsionnykh gazoturbinnykh dvigatelei (Design of Aircraft Gas Turbine Engines), Samara: Izd. SNTs RAN, 2008.

    Google Scholar 

  4. Petrov, V.N., Analysis of the Sensitivity of Aerodynamic Characteristics of the Flow Structure of Co-Flowing Jet in the Channel to ANSYS Fluent Parameters, Vestnik KNITU, 2016, vol. 19, no. 19, pp. 16–19.

    Google Scholar 

  5. Varsegov, V.L. and Shabalin, A.S., Selection of an Optimal Turbulence Model for Numerical Flow Simulation in a Cascade Type Turbofan Engine Thrust Reverser, Izv. Vuz. Av. Tekhnika, 2015, vol. 58, no. 4, pp. 117–120 [Russian Aeronautics (Engl. Transl.), 2015, vol. 58, no. 4, pp. 484–487].

    Google Scholar 

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Authors and Affiliations

  1. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, 420111 Tatarstan, Russia

    V. L. Varsegov

  2. All-Russia Research Institute of Flow Metering (FGUP VNIIR), ul. Vtoraya Azinskaya 7a, Kazan, 420088 Tatarstan, Russia

    A. S. Shabalin

Authors
  1. V. L. Varsegov
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  2. A. S. Shabalin
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Corresponding author

Correspondence to V. L. Varsegov.

Additional information

Original Russian Text© V.L. Varsegov, A.S. Shabalin, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika, 2017, No. 2, pp. 43–49.

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Varsegov, V.L., Shabalin, A.S. Numerical determination of the gas-dynamic behavior of vane cascades with various deflection angles of the trailing edges of longitudinal ribs of an advanced gas-turbine engine thrust reverser. Russ. Aeronaut. 60, 206–213 (2017). https://doi.org/10.3103/S1068799817020076

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  • DOI: https://doi.org/10.3103/S1068799817020076

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