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Use of the RANS/ILES Method to Study the Efficiency of Synthetic Jet Application for Flow Control in an S-Shaped Intake Integrated with an Airframe

  • HEAT AND MASS TRANSFER AND PHYSICAL GASDYNAMICS
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High Temperature Aims and scope

Abstract

The flow in the subsonic S-shaped air intake with a D-shaped inlet and circular outlet cross sections is calculated with the combined high-resolution RANS/ILES method. A flat plate, on which the air intake is mounted, is used as an airframe simulator. The boundary layer is specified at the beginning of the plate, and its profile is close to the profile of the turbulent boundary layer. The calculations were performed on a structured grid containing 7 × 106 cells; good agreement with the experiment data is obtained. The causes of large flow nonuniformities at the outlet of air intake are revealed; the efficiency of the use of synthetic jets to improve its characteristics is studied. The influence of the regime parameters of synthetic jets and the location of slots for their egress on the air-intake flow is analyzed.

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REFERENCES

  1. Berrier, B.L., Carter, M.B., and Allan, B.G., High reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion, NASA/TP, 2005, no. 213766.

  2. Xingya, D., Zhaolin, F., Jianchao, F., Liquan, Z., Wei, R., and Run, Z., Chin. J. Aeronaut., 2015, vol. 28, no. 5, p. 1381.

    Article  Google Scholar 

  3. Shu, S. and Rongwei, G., Chin. J. Aeronaut., 2006, vol. 19, no. 1, p. 10.

    Article  Google Scholar 

  4. Anderson, B.H. and Keller, D.J., Considerations in the measurement of inlet distortion for high cycle fatigue in compact inlet diffusers, NASA-TM, 2002, no. 211476.

  5. Harouni, A.G., Aerosp. Sci. Technol., 2014, vol. 39, p. 472.

    Article  Google Scholar 

  6. Gorton, S.A., Owens, L.R., Luther, N., Jenkins, L.N., Brian, G., Allan, B.G., and Schuster, E.P., Active flow control on a boundary-layer-ingesting inlet, AIAA Paper no. 2004-1203, 2004.

  7. Johnson, B.C., Webster, R.S., and Sreenivas, K., A numerical investigation of s-duct flows with boundary-layer ingestion, AIAA Paper no. 2010-841, 2010.

  8. Lee, B.J. and Liou, M.S., Re-design of boundary-layer-ingesting offset inlet via passive flow control, AIAA Paper no. 2010-842, 2010.

  9. Wellbom, S.R. and Okiishi, T.H., A study of the compressible flow through a diffusing S-duct, NASA-TM, 1993, no. 106411.

  10. Keerthi, M.C. and Kushari, A., Aerosp. Sci. Technol., 2014, vol. 34, p. 12.

    Article  Google Scholar 

  11. Yu, J.Y., Liu, H.P., Liu, L., Li, G.Z., Chen, F., and Song, Y.P., Numerical investigation on influence of suction in S-shaped inlet to the rear fan-stage performance, AIAA Paper no. 2016-5055, 2016.

  12. Gissen, A.N., Vukasinovic, B., McMillan, M.L., and Glezer, A., Distortion management in a BLI inlet diffuser using synthetic-jet hybrid flow control, AIAA Paper no. 2011-0035, 2011.

  13. Gissen, A.N., Vukasinovic, B., and Glezer, A., Manipulation of streamwise vorticity in an emulated diffuser boundary layer using hybrid flow control, AIAA Paper no. 2010-4586, 2010.

  14. Aram, S. and Mittal, R., Int. J. Flow Control, 2011, vol. 3, nos. 2–3, p. 87.

    Article  Google Scholar 

  15. Lyubimov, D.A., High Temp., 2011, vol. 49, no. 4, p. 539.

    Article  Google Scholar 

  16. Lyubimov, D., Makarov, A., and Potekhina, I., in Proc. 28th Int. Congress of the Aeronautical Science, Brisbane, 2012.

  17. Lyubimov, D.A. and Potekhina, I.V., Fluid Dyn., 2015, vol. 50, no. 4, p. 590.

    Article  Google Scholar 

  18. Lyubimov, D.A., High Temp., 2012, vol. 50, no. 3, p. 420.

    Article  Google Scholar 

  19. Remeev, N.Kh., Aerodinamika vozdukhozabornikov sverkhzvukovykh samoletov (Aerodynamics of the Air Intakes of Supersonic Aircraft), Zhukovskii: Tsentr. Aerogidrodin. Inst. im. N.E. Zhukovskogo, 2002.

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Funding

This work was supported in part by the Russian Foundation for Basic Research, grant no. 18-08-00271.

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Authors and Affiliations

  1. Baranov Central Institute of Aviation Motor Development, 111116, Moscow, Russia

    L. A. Benderskii, D. A. Lyubimov & A. A. Terekhova

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  1. L. A. Benderskii
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  2. D. A. Lyubimov
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  3. A. A. Terekhova
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Correspondence to D. A. Lyubimov.

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Translated by M. Samokhina

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Benderskii, L.A., Lyubimov, D.A. & Terekhova, A.A. Use of the RANS/ILES Method to Study the Efficiency of Synthetic Jet Application for Flow Control in an S-Shaped Intake Integrated with an Airframe. High Temp 58, 266–277 (2020). https://doi.org/10.1134/S0018151X20020030

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  • DOI: https://doi.org/10.1134/S0018151X20020030

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