Skip to main content

Reduction of Turbulent Boundary Layer Noise with Actively Controlled Carbon Fiber Reinforced Plastic Panels

  • Chapter
  • First Online:
Adaptive, tolerant and efficient composite structures

Part of the book series: Research Topics in Aerospace ((RTA))

  • 2690 Accesses

Abstract

The turbulent boundary layer (TBL) is one of the dominant external noise sources in high subsonic aircrafts. Especially in modern aircrafts where common materials for fuselages are currently substituted by carbon-fiber-reinforced-plastics (CFRP), it is essential to avoid a decrease of passenger comfort as a result of an inferior transmission loss of the new materials. To increase the transmission loss of CFRP panels they are equipped with active noise reduction systems. In this paper the results of an experimental study in the aeroacoustic wind tunnel of the German Aerospace Center (DLR) are presented. An active panel excited by a TBL is tested at flow speeds up to Mach 0.16. The CFRP panel (500 × 800 × 2.7 mm3) is equipped with five piezo-ceramic patch actuators and ten accelerometers. Active structural acoustic control (ASAC) and active vibration control (AVC) are used to reduce the broadband TBL noise transmission in the bandwidth from 1 to 500 Hz. Feedforward (FF) and feedback (FB) control algorithms are applied in the experiments and show high performance even in presence of plant uncertainties. To improve control results the generalized plant framework of robust control is utilized for global feedback control. Finally, an overview of the achieved results is given.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 84.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 109.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 109.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. Wilby, J.F.: Aircraft interior noise. J. Sound Vib. 190(3), 545–564 (1996)

    Article  Google Scholar 

  2. Corcos, G.M.: The structure of the turbulent pressure field in boundary-layer flows. J. Fluid Mech. 18, 353–378 (1964)

    Article  MATH  Google Scholar 

  3. Gibbs, G.P., Cabell, R.H.: Active control of turbulent boundary layer induced sound radiation from multiple aircraft panels. In: Proceedings of 8th AIAA/CEAS Aeroacoustics Conference, Breckenridge, CO (2002)

    Google Scholar 

  4. Schiller, N.H., Fuller, C.R.: A high-authority/low-authority control strategy for coupled aircraft-style bays. In: Proceedings of ACTIVE 2006, Adelaide, Australia (2006)

    Google Scholar 

  5. Rohlfing, J., Gardonio, P.: Homogeneous and sandwich active panels under deterministic and stochastic excitation. J. Acoust. Soc. Am. 125(6), 3696–3706 (2009)

    Article  Google Scholar 

  6. Thomas, D.R., Nelson, P.A.: Feedback control of sound radiation from a plate excited by a turbulent boundary layer. J. Acoust. Soc. Am. 98(5), 2651–2662 (1995)

    Article  Google Scholar 

  7. Maury, C., Gardonio, P., Elliott, S.J.: Model for active control of flow-induced noise transmitted through double partitions. AIAA J. 40, 1113–1121 (2002)

    Article  Google Scholar 

  8. Heintze, O., Rose, M., Algermissen, S., Misol, M.: Development and experimental application of a pre-design tool for active noise and vibration reduction systems. In: Proceedings of ACTIVE 2009, Ottawa, Canada (2009)

    Google Scholar 

  9. Ewert, R.: Rpm––the fast random particle-mesh method to realize unsteady turbulent sound sources and velocity fields for caa applications. In: Proceedings of 13th AIAA/CEAS Aeroacoustics Conference. http://elib.dlr.de/52932/ (2007)

  10. Siefert, M., Ewert, R. (2009), Anisotropic synthetic turbulence with sweeping generated by random particle-mesh method. In: Peinke, J., Oberlack, M., Talamelli, A. (eds.) Progress in Turbulence III: Proceedings of the iTi Conference in Turbulence, p. 143

    Google Scholar 

  11. Katayama, T.: Subspace Methods for System Identification. Springer, London (2005)

    MATH  Google Scholar 

  12. Algermissen, S., Rose, M., Keimer, R., Monner, H.P., Breitbach, E.: Automated synthesis of robust controllers for smart-structure applications in parallel robots. In: Proceedings of AIAA/ASME/AHS Adaptive Structures Conference, Honolulu, USA (2007)

    Google Scholar 

  13. Algermissen, S., Rose, M., Keimer, R., Sinapius, M.: Robust gain-scheduling for smart-structures in parallel robots. In: 16th Annual International Symposium on Smart Structures and Materials, SPIE, San Diego (2009)

    Google Scholar 

  14. Elliott, S.: Signal Processing for Active Control. Academic Press, London (2001)

    Google Scholar 

  15. Kuo, S.M., Morgan, D.R.: Active Noise Control Systems. John Wiley & Sons, New York (1996)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Stephan Algermissen .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2013 Springer-Verlag Berlin Heidelberg

About this chapter

Cite this chapter

Algermissen, S., Misol, M., Unruh, O. (2013). Reduction of Turbulent Boundary Layer Noise with Actively Controlled Carbon Fiber Reinforced Plastic Panels. In: Wiedemann, M., Sinapius, M. (eds) Adaptive, tolerant and efficient composite structures. Research Topics in Aerospace. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-29190-6_34

Download citation

  • DOI: https://doi.org/10.1007/978-3-642-29190-6_34

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-29189-0

  • Online ISBN: 978-3-642-29190-6

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics