Skip to main content

Direct and Large-Eddy Simulation of a Transitional Rectangular Jet

  • Chapter
Direct and Large-Eddy Simulation IV

Part of the book series: ERCOFTAC Series ((ERCO,volume 8))

Abstract

The transition of a Mach 0.5 rectangular jet with a nozzle aspect ratio of five and a Reynolds number of 2000 based on the narrow nozzle width was computed with DNS and LES based on the Approximate Deconvolution Model (Stolz and Adams, 1999). The DNS data are used for validating the LES. The transition process of the jet is well reproduced by the LES and mean flow data show good agreement with the DNS data.

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 169.00
Price excludes VAT (USA)
  • Available as 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

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  • Adams, N. A. and Shariff, K. (1996). A high resolution hybrid compact-eno scheme for shock-turbulence interaction problems. J. Comput. Phys., 127: 27–51.

    Article  MathSciNet  MATH  Google Scholar 

  • Gutmark, E. J. and Grinstein, F. F. (1999). Flow control with noncircular jets. Ann. Rev. Fluid Mech., 31: 239–72.

    Article  Google Scholar 

  • Lele, S. K. (1992). Compact finite difference schemes with spectral-like resolution. J. Comput. Phys., 103: 16–42.

    Article  MathSciNet  MATH  Google Scholar 

  • Rembold, B., Adams, N. A., and Kleiser, L. (2001). Direct numerical simulation of a transitional rectangular jet. In Proceedings of the 2nd International Symposium on Turbulence and Shear Flow Phenomena (TSFP2), Stockholm, June 27–29.

    Google Scholar 

  • Stolz, S. and Adams, N. A. (1999). An approximate deconvolution procedure for large-eddy simulation. Phys. Fluids, 11(7):1699–1701.

    Google Scholar 

  • Stolz, S., Adams, N. A., and Kleiser, L. (2001a). An approximate deconvolution model for large-eddy simulation with application to incompressible wall-bounded flows. Phys. Fluids, 13 (4): 997–1015.

    Article  Google Scholar 

  • Stolz, S., Adams, N. A., and Kleiser, L. (2001b). The approximate deconvolution model for LES of compressible flows and its application to shock-turbulent-boundarylayer interaction. To appear in Phys. Fluids.

    Google Scholar 

  • Yu, M.-H. and Monkewitz, P. A. (1990). The effect on nonuniform density on the absolute instability of two-dimensional inertial jets and wakes. Phys. Fluids, A2(7): 11751181.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2001 Springer Science+Business Media Dordrecht

About this chapter

Cite this chapter

Rembold, B., Adams, N.A., Kleiser, L. (2001). Direct and Large-Eddy Simulation of a Transitional Rectangular Jet. In: Geurts, B.J., Friedrich, R., Métais, O. (eds) Direct and Large-Eddy Simulation IV. ERCOFTAC Series, vol 8. Springer, Dordrecht. https://doi.org/10.1007/978-94-017-1263-7_24

Download citation

  • DOI: https://doi.org/10.1007/978-94-017-1263-7_24

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-90-481-5893-5

  • Online ISBN: 978-94-017-1263-7

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics