Skip to main content

Study About Boundary-Layer Suction at a Juncture for Sustained Laminar Flow

  • Conference paper
  • First Online:

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ((NNFM,volume 136))

Abstract

Two-dimensional direct numerical simulations (DNS) are used to study the influence of active and passive suction at the juncture between two wing elements on laminar-turbulent transition. Suction is applied through the juncture’s gap in front of a forward-facing step. For first, fundamental investigations, the juncture is located in a compressible flat-plate boundary-layer flow without streamwise pressure gradient. To quantify the impact of suction on laminar-turbulent transition, N-factors are calculated. For this, the growth of introduced Tollmien-Schlichting (TS) waves is evaluated according to the \(e^N\) method. Depending on the perilousness of juncture shapes, suction is capable or incapable to compensate their negative impact on laminar-turbulent transition. In addition to active suction, a method allowing passive suction is presented. The work concludes with a discussion about possible integrations of suction at aerodynamic elements, in particular at wings.

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

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   169.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   219.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD   219.99
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

Learn about institutional subscriptions

References

  1. Edelmann, C.A., Rist, U.: Impact of forward-facing steps on laminar-turbulent transition in transonic flows. AIAA J. https://doi.org/10.2514/1.J053529 (2015)

  2. Havar, T., Geistbeck, M., Meyer, M., Rohr, O., Meer, T.: Connection arrangement for connecting two profiled elements in an aerodynamically smooth manner, method for producing said connection arrangement, and device for carrying out the method. World Intellectual Property Organization, WIPO, Internationales Patent, WO 2013/000447 A1 (2013)

    Google Scholar 

  3. Hühne, C., Ückert, C., Steffen, O.: Multifunktionale Flügelvorderkante in Multimaterialbauweise. Lightweight Design, Ausgabe 1/2016 (2016)

    Google Scholar 

  4. van Ingen J.L.: A suggested semi-empirical method for the calculation of the boundary layer transition region. Technische Hogeschool Delft, Internal report, Rapport VTH-74 (1956)

    Google Scholar 

  5. Perraud, J., Arnal, D., Kuehn, W.: Laminar-turbulent transition prediction in the presence of surface imperfections. J. Eng. Syst. Model. Simul. https://doi.org/10.1504/IJESMS.2014.063129 (2014)

  6. Zahn, J., Rist, U.: Impact of deep gaps on laminar-turbulent transition in compressible boundary-layer flow. AIAA J. https://doi.org/10.2514/1.J054112 (2016)

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Johannes Zahn .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2018 Springer International Publishing AG

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Zahn, J., Rist, U. (2018). Study About Boundary-Layer Suction at a Juncture for Sustained Laminar Flow. In: Dillmann, A., et al. New Results in Numerical and Experimental Fluid Mechanics XI. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 136. Springer, Cham. https://doi.org/10.1007/978-3-319-64519-3_32

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-64519-3_32

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-64518-6

  • Online ISBN: 978-3-319-64519-3

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics