Skip to main content
SpringerLink
Log in

Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence

  • Conference paper
  • First Online:
Advances in Simulation of Wing and Nacelle Stall (FOR 1066 2014)

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ((NNFM,volume 131))

Included in the following conference series:

Abstract

The work here presents an experimental and computational study of a simplified intake bottom lip at incidence. The experiments are carried out in a small-scale blow-down wind tunnel. Computations are carried out in parallel to experiments using an in-house unstructured compressible flow solver. Evaluation of current Reynolds Averaged Navier-Stokes (RANS) methods are conducted and compared to experimental measurements. Qualitative results show good agreement of experiments to the computations, although further analysis is required. Current computational strategies follow a steady, quasi-two-dimensional approach, with fully structured wall-resolved grids.

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

Access this chapter

Log in via an institution
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 PDF
  • Read on any device
  • Instant download
  • Own it forever
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

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Babinsky, H., Harvey, J.: Shock Wave-Boundary-Layer Interactions. Cambridge University Press (2011)

    Google Scholar 

  2. Bruce, P.J.K., Burton, D.M.F., Titchener, N.A., Babinsky, H.: Corner effect and separation in transonic channel flows. Journal of Fluid Mechanics 679, 247–262 (2011)

    Google Scholar 

  3. Colliss, S.P.: Vortical structures on three-dimensional shock control bumps, PhD thesis, University of Cambridge (2014)

    Google Scholar 

  4. Lapworth, L.: Hydra-cfd: A framework for collaborative cfd development, International Conference on Scientific and Engineering Computation (IC-SEC), Singapore (2004)

    Google Scholar 

  5. Seddon, J.: Intake Aerodynamics, Blackwell Publishing (1999)

    Google Scholar 

  6. Spalart, P.R., Allmaras, S.R.: A one-equation turbulence model for aerodynamic flows. La Recherche Aerospatiale 1, 5–21 (1994)

    Google Scholar 

  7. Titchener, N.A.: An Experimental Investigation of Flow Control for Supersonic Inlets, PhD thesis, University of Cambridge (2013)

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Department of Engineering, University of Cambridge, Cambridge, UK

    Tafara E. Makuni, Hardeep S. Kalsi, Paul G. Tucker & Holger Babinsky

Authors
  1. Tafara E. Makuni
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Hardeep S. Kalsi
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Paul G. Tucker
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. Holger Babinsky
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Tafara E. Makuni .

Editor information

Editors and Affiliations

  1. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

    Rolf Radespiel

  2. Institute of Jet Propulsion, Universität der Bundeswehr München, Neubiberg, Germany

    Reinhard Niehuis

  3. Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Braunschweig, Germany

    Norbert Kroll

  4. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

    Kathrin Behrends

Rights and permissions

Reprints and permissions

Copyright information

© 2016 Springer International Publishing Switzerland

About this paper

Cite this paper

Makuni, T.E., Kalsi, H.S., Tucker, P.G., Babinsky, H. (2016). Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence. In: Radespiel, R., Niehuis, R., Kroll, N., Behrends, K. (eds) Advances in Simulation of Wing and Nacelle Stall. FOR 1066 2014. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 131. Springer, Cham. https://doi.org/10.1007/978-3-319-21127-5_19

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-21127-5_19

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-21126-8

  • Online ISBN: 978-3-319-21127-5

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics

Search

Navigation