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Vibroacoustics Under Aerodynamic Excitations

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Abstract

This paper gives a number of energy considerations related to the flow induced vibration and noise predictions. In this context, reduced modeling of structural-acoustic issues are the main red line of the work. The present paper deals thus with equivalent “rain on the roof” (ROF) excitations, which allow the modeling of spatially correlated broadband sources by statistically independent point forces. ROF excitation largely simplifies the expressions of the joint acceptance functions and can be easily modeled using finite element method (FEM). Two approaches are presented here and an equivalent model of excitation is developed and validated on acoustic and aerodynamic excitations, such as diffuse field or turbulent boundary layer (TBL) excitations. The first idea, considers the equivalence over the extended physical domain. It allows equivalent ROF excitation only for frequencies over the acoustic coincidence effect. The second method is based on the wavenumber space equivalence. Validation of this approach has been carried out for different acoustic and aerodynamic excitations, and for different structural boundary conditions. Numerical experiments show that this approach gives acceptable results for a wide frequency range specifically for TBL excitations. Then, the problem of the structural–acoustic response under aerodynamic sources is considered further. The structure is a composite structure of arbitrary thickness and anisotropy. The fully coupled system is modeled using a Statistical Energy Analysis like (SEA-like) approach, and the energetic characteristics for each subsystem are computed and compared to the direct FEM solution. The error of the reduced model calculations for each frequency band is presented and the limits of the reliability of the reduction are explored. Different strategies concerning the reduction process parameters are investigated in order to optimize the accuracy with respect to time efficiency. The loading applied to the model comprises typical random distributed excitations, such as a ‘rain-on-the-roof’ excitation, a diffused sound field and a Turbulent Boundary Layer (TBL) excitation.

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Notes

  1. 1.

    SEALASCAR is an SEA based code developed and employed by EADS Space Transportation [15, 19] for ARIANE vibroacoustic design.

References

  1. G.M. Corcos, Resolution of pressure in turbulence. J. Acoust. Soc. Am. 35(2) (1963)

    Google Scholar 

  2. D.M. Chase, Modelling the wavevector-frequency spectrum of turbulent boundary layer wall-pressure. J. Sound Vib. 70, 29–67 (1980)

    Article  MATH  Google Scholar 

  3. B.M. Efimstov, Characteristics of the field of turbulent wall pressure fluctuations at large Reynolds numbers. Sov. Pysics—Acoust. 28(4), 289–292 (1992)

    Google Scholar 

  4. W.R. Graham, A comparison of models for the wavenumber-frequency spectrum of turbulent boundary layer pressures. J. Sound Vib. 206(4), 541–565 (1997)

    Article  Google Scholar 

  5. R.H. Lyon, R. Dejong, Theory and Application of Statistical Energy Analysis, 2nd edn. (Butterworth Heinemann, Newton, 1995)

    Google Scholar 

  6. R.S. Langley, P.G. Bremner, A hybrid method for the vibration analysis of complex structural-acoustic systems. J. Acoust. Soc. Am. 105, 1657–1671 (1999)

    Article  Google Scholar 

  7. B. Mace, Statistical energy analysis: coupling loss factors, indirect coupling and system modes. J. Sound Vib. 279(1–2), 141–170 (2005)

    Article  MathSciNet  Google Scholar 

  8. C.R. Fredö, Statistical energy analysis and the individual case. PhD thesis, Chalmers University of Technology, 1995

    Google Scholar 

  9. B. Hiverniau, Transmissions solidiennes: méthodologie de prévision vibroacoustique moyennes et hautes fréquences sous excitations aéroacoustiques, (Structural vibration transmission: mid-high frequency approaches under aerodynamic excitations). PhD thesis, Ecole Centrale de Lyon, 2007

    Google Scholar 

  10. G. Maidanik, Response of ribbed panels to reverberant acoustic fields. J. Acoust. Soc. Am. 34(6) (1962)

    Google Scholar 

  11. S. Finnveden, F. Birgersson, U. Ross, T. Kremer, A model of wall pressure correlation for prediction of turbulence-induced vibration. J. Fluids Struct. 20, 1127–1143 (2005)

    Article  Google Scholar 

  12. G. Maidanik, Use of delta function for the correlations of pressure fields. J. Acoust. Soc. Am. 33(11), 1598–1606 (1961)

    Article  Google Scholar 

  13. J. Park, T. Siegmund, L. Mongeau, Analysis of the flow-induced vibrations of viscoelastically supported rectangular plates. J. Sound Vib. 261, 225–245 (2003)

    Article  Google Scholar 

  14. S.J. Elliot, P. Gardonio, C. Maury, A feasibility study for the laboratory simulation of turbulent boundary layer pressure fields, in 7th AIAA/CEAS Aeronautics Conference, Maastricht, Netherlands, 28–30 May 2001

    Google Scholar 

  15. B. Troclet, Manuel théorique LASCAR. EADS Launch Vehicles (1987)

    Google Scholar 

  16. C. Maury, P. Gardonio, S.J. Elliot, A wavenumber approach to modeling the response of a randomly excited panel, part I: general theory. J. Sound Vib. 252(1), 83–113 (2002)

    Article  Google Scholar 

  17. F. Birgersson, S. Finnveden, A spectral element for modeling of plate vibration. Part 2: turbulence excitation. J. Sound Vib. 287, 315–328 (2005)

    Article  Google Scholar 

  18. S.A. Hambric, Y.F. Hwang, W.K. Bonness, Vibrations of plates with clamped and free edges excited by low-speed turbulent boundary layer. J. Fluid Sand Struct. 19, 93–110 (2004)

    Article  Google Scholar 

  19. S. De Rosa, F. Franco, Exact and numerical responses of a plate under a turbulent boundary layer excitation. J. Fluids Struct. 24, 212–230 (2008)

    Article  Google Scholar 

  20. B. Troclet, M. Depuydt, P. Gonzalez, Experimental analysis of the aerodynamic noise on the Ariane 5 Launch Vehicle Upper Part, in Ariane 5 Structures et Technologies, Cépaduès–Editions (1993), pp. 515–526

    Google Scholar 

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Correspondence to Mohamed N. Ichchou .

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Ichchou, M.N., Bareille, O., Troclet, B., Hiverniau, B., De Rochambeau, M., Chronopoulos, D. (2015). Vibroacoustics Under Aerodynamic Excitations. In: Ciappi, E., De Rosa, S., Franco, F., Guyader, JL., Hambric, S. (eds) Flinovia - Flow Induced Noise and Vibration Issues and Aspects. Springer, Cham. https://doi.org/10.1007/978-3-319-09713-8_11

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  • DOI: https://doi.org/10.1007/978-3-319-09713-8_11

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-09712-1

  • Online ISBN: 978-3-319-09713-8

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