Experimental Investigations on the Effect of Dielectric Barrier Discharge on the Hypersonic Flow Around a Flat Plate

  • Conference paper
28th International Symposium on Shock Waves

Introduction

Surface dielectric barrier discharges (DBD) are known to offer potential flow control techniques for low speed flows. A well known application of DBD in low speed flows is separation control as illustrated by Little et al. [1]. For high speed flows (supersonic and hypersonic flows) there is a need for deeper understanding of their nature of interaction and applicability. Literature on low speed flows suggests the body force field created by DBD, as the reason for flow alteration (Boeuf and Pitchford [2]). High speed flows, hypersonic flows in particular, are characterized by high flow kinetic energy, and thus one cannot ignore the possible energy interactions the flow can have with the regions of high temperature in the field (as may be the case with discharge).

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

Access this chapter

Subscribe and save

Springer+ Basic
EUR 32.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or Ebook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 259.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 329.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free ship** worldwide - see info
Hardcover Book
USD 329.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free ship** worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

Similar content being viewed by others

References

  1. Little, J., Nishihara, M., Adamovich, I., Samimy, M.: High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator. Exp. Fluids 48, 521–537 (2010)

    Article  Google Scholar 

  2. Boeuf, J.P., Pitchford, L.C.: Electro-hydrodynamic force and aerodynamic flow acceleration in surface dielectric barrier discharge. Journal of Applied Physics 97(103307), 1–10 (2005)

    Google Scholar 

  3. Satheesh, K., Jagadeesh, G.: Effect of concentrated energy deposition on the aerodynamic drag of a blunt body in hypersonic stream. Physics of Fluids 19(031701), 1–4 (2007)

    Google Scholar 

  4. Yan, H., Gaitonde, D.: Effect of thermally induced perturbation in supersonic boundary layers. Physics of Fluids 22(064101), 1–16 (2010)

    Google Scholar 

  5. Pavon, S., Dorier, J.-L., Hollenstein, C., Ott, P., Leyland, P.: Effects of high-speed airflows on a surface dielectric barrier discharge. J. Phys. D: Appl. Phys. 40, 1733–1741 (2007)

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2012 Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Sriram, R., Jagadeesh, G., Reddy, K.P.J. (2012). Experimental Investigations on the Effect of Dielectric Barrier Discharge on the Hypersonic Flow Around a Flat Plate. In: Kontis, K. (eds) 28th International Symposium on Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25685-1_149

Download citation

  • DOI: https://doi.org/10.1007/978-3-642-25685-1_149

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-25684-4

  • Online ISBN: 978-3-642-25685-1

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics

Navigation