Skip to main content

Numerical Simulation of the Turbulent Flow Around a Wing

  • Conference paper
  • First Online:
  • 1767 Accesses

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

Abstract

The turbulent flow around a wing in the atmospheric boundary layer is simulated. For initialising the turbulent wind field a synthetic turbulence generator is used. The turbulence generator generates a 3D turbulent field which matches important statistics from measurement data. In the results of the simulation an influence of the grid and turbulence mode on the resolved turbulent flow was observed. In general there is a decrease of resolved turbulent kinetic energy in the smaller scales when the turbulence leaves the Cartesian grid and enters the unstructured grid around the wing. In the analysis of the spectra of the aerodynamic forces it could be seen that only the largest scales of the turbulence have a significant effect on the aerodynamics of the wing. The results are preliminary, however, since the simulation is not yet finished and the analysis is not complete yet.

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 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

Learn about institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Doligalski: Vortex Interactions With Walls. Annu. Rev. Fluid Mech. 26, 573–616 (1994)

    Google Scholar 

  2. Brandt, L., Schlatter, P., Henningson, D.S.: Transition in boundary layers subject to free-stream turbulence. J. Fluid Mech. 517, 167–198 (2004)

    Article  MathSciNet  MATH  Google Scholar 

  3. Kelleners, P., Heinrich, R.: Simulation of Interaction of Aircraft with Gust and Resolved LES-Simulated Atmospheric Turbulence. In: Simulation of Wing and Nacelle Stall. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer (2015)

    Google Scholar 

  4. Heinrich, R.: Simulation of Interaction of Aircraft and Gust Using the TAU-Code. New Results in Numerical and Experimental Fluid Mechanics IX, Notes on Numerical Fluid Mechanics and Multidisciplinary Design 124, 503–511 (2014)

    Article  Google Scholar 

  5. Auerswald, T., Bange, J., Knopp, T., Weinman, K., Radespiel, R.: Large-Eddy Simulations of realistic atmospheric turbulence with the DLR-TAU-code initialized by in situ airborne measurements. Computers & Fluids 66, 121–129 (2012)

    Article  Google Scholar 

  6. Knigge, C., Auerswald, T., Raasch, S., Bange, J.: Comparison of two methods simulating highly resolved atmospheric turbulence data for study of stall effects. Computers & Fluids 108, 57–66 (2015)

    Article  Google Scholar 

  7. Schwamborn D., Gerhold T., Heinrich R.: The DLR TAU-Code: Recent Applications in Research and Industry. ECCOMAS CFD 2006 (2006)

    Google Scholar 

  8. Deardorff, J.W.: A Numerical Study of Three-Dimensional Turbulent Channel Flow at Large Reynolds Numbers. J. Fluid Mech. 41, 453–480 (1970)

    Article  Google Scholar 

  9. Gerhold, T., Friedrich, O., Evans, J., Galle, M.: Calculation of Complex Three Dimensional Configurations Employing the DLR-TAU-Code. AIAA-paper 97–0167 (1997)

    Google Scholar 

  10. Spalart, P.R., Jou, W.H., Strelets, M., Allmaras, S.R.: Comments on the feas1ibility of LES for wings, and on a hybrid RANS/LES approach. In: Proceedings of First AFOSR International Conference on DNS/LES (1997)

    Google Scholar 

  11. Bange, J., Spie, T., van den Kroonenberg, A.: Characteristics of the Early-Morning Shallow Convective Boundary Layer from Helipod Flights during STINHO-2. Theor. Appl. Climatol 90, 113–126 (2007)

    Google Scholar 

  12. Lund, T.S., Wu, X., Squires, K.D.: Generation of Turbulent Inflow Data for Spatially-Developing Boundary Layer Simulations. J. Comput. Phys. 140, 233–258 (1998)

    Article  MathSciNet  MATH  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Torsten Auerswald .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2016 Springer International Publishing Switzerland

About this paper

Cite this paper

Auerswald, T., Bange, J. (2016). Numerical Simulation of the Turbulent Flow Around a Wing. 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_14

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-21127-5_14

  • 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