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The Acoustic Impact on Aviation Aggregates Made of Polymer Composite Materials

  • RELIABILITY, STRENGTH, AND WEAR RESISTANCE OF MACHINES AND STRUCTURES
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Abstract

The features of the acoustic impact on aircraft aggregates made of polymer composite materials are investigated. A technique for setting the wave angle is described; it equalizes the scale factors of both measuring channels of the differential aggregate made of polymer composite materials and compensates for the cross-damping error. Analytical expressions are obtained for the scale factor and the zero offset of the differential aggregate made of polymer composite materials. This scale factor, in contrast to the discrete noise oscillation mode, does not depend on the resonant oscillation amplitude and frequency. The operating mode of the aggregate made of polymer composite materials is shown to have an ability to compensate for the resonator frequency difference, when measuring the angular velocity, by means of the control system.

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REFERENCES

  1. Adam, A., Papamoschou, D., and Bogey, C., Imprint of vortical structures on the near-field pressure of a turbulent jet, AIAA J., 2022, vol. 60, no. 3, pp. 1578–1591. https://doi.org/10.2514/1.J061010

    Article  Google Scholar 

  2. Gangipamula, R., Ranjan, P., and Patil, R.S., Study on fluid dynamic characteristics of a low specific speed centrifugal pump with emphasis on trimming operations, Int. J. Heat Fluid Flow, 2022, vol. 95, p. 108952. https://doi.org/10.1016/j.ijheatfluidflow.2022.108952

    Article  Google Scholar 

  3. Liu, J., Cong, S., Song, Y., Chen, S., and Wu, D., Flow structure and acoustics of underwater imperfectly expanded supersonic gas jets, Shock Waves, 2022, vol. 32, pp. 283–294. https://doi.org/10.1007/s00193-021-01069-9

    Article  Google Scholar 

  4. Nikam, Sh.R. and Sharma, Sh., Correlation in the near and far field of compressible jet to identify noise source characteristics, Flow, Turbul. Combust., 2022, vol. 108, no. 3, pp. 739–773. https://doi.org/10.1007/s10494-021-00299-2

    Article  Google Scholar 

  5. Niki, Y., Rajasegar, R., Li, Z., Musculus, M.P.B., Garcia Oliver, J.M., and Takasaki, K., Verification of diesel spray ignition phenomenon in dual-fuel diesel-piloted premixed natural gas engine, Int. J. Engine Res., 2022, vol. 23, no. 2, pp. 180–197. https://doi.org/10.1177/1468087420983060

    Article  Google Scholar 

  6. Rego, L., Avallone, F., Ragni, D., and Casalino, D., On the mechanisms of jet-installation noise reduction with flow-permeable trailing edges, J. Sound Vib., 2022, vol. 520, p. 116582. https://doi.org/10.1016/j.jsv.2021.116582

    Article  Google Scholar 

  7. Varé, M. and Bogey, C., Generation of acoustic tones in round jets at a Mach number of 0.9 impinging on a plate with and without a hole, J. Fluid Mech., 2022, vol. 936, p. A16. https://doi.org/10.1017/jfm.2022.47

    Article  MathSciNet  MATH  Google Scholar 

  8. Wang, X., Lian, J., Ma, B., and Du, S., Numerical simulations and predictions of low-frequency noises downstream spillway tunnel, J. Hydroelectr. Eng., 2022, vol. 41, no. 1, pp. 103–112. https://doi.org/10.11660/slfdxb.20220111

    Article  Google Scholar 

  9. Webb, N., Esfahani, A., Leahy, R., and Samimy, M., Active control of rectangular supersonic twin jets using perturbations: Effects and mechanism, AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum, San Diego, Calif., 2022, AIAA, 2022, p. 2022-2401. https://doi.org/10.2514/6.2022-2401

  10. Zaman, K.B.M.Q., Fagan, A.F., and Upadhyay, P., Pressure fluctuations due to ‘trapped waves’ in the initial region of compressible jets, J. Fluid Mech., 2022, vol. 931, p. A30. https://doi.org/10.1017/jfm.2021.954

    Article  MathSciNet  MATH  Google Scholar 

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Correspondence to V. S. Oleshko or Ying Sun.

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FINANCING

This work is supported by the following grants: Natural Science Foundation of Shaanxi Province, project no. 2021JQ 081, and the Basic Research Programs of Taicang, project no. TC2020JC14.

CONFLICT OF INTEREST

The authors declare that they have no conflicts of interest.

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Translated by I. Dikhter

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Sha, M., Goncharenko, V.I., Yurov, V.M. et al. The Acoustic Impact on Aviation Aggregates Made of Polymer Composite Materials. J. Mach. Manuf. Reliab. 52, 38–45 (2023). https://doi.org/10.3103/S1052618823010119

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  • DOI: https://doi.org/10.3103/S1052618823010119

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