Skip to main content

Experimental and numerical investigation of high enthalpy flow past a cylinder in HEG

  • Conference paper
  • First Online:
Shock Waves

Abstract

Basic aerodynamic configurations are well suited to study fundamental aspects of high enthalpy flows. A test campaign of the flow around a cylinder has been performed in the High Enthalpy Shock Tunnel Göttingen HEG. Measurements of density distributions in the shock layer as well as surface pressure and heat flux were taken. The flow in the shock layer is subjected to various relaxation phenomena and therefore, the presented measurements provide a useful basis for the validation of physico-chemical models used in CFD codes. This paper presents results of the test campaign and comparisons of measurements to numerical computations. The sensitivity of the CFD results to different parameters of physico-chemical models will be discussed.

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 299.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever

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. S. Brück, R. Radespiel, J.M.A. Longo: Comparison of nonequilibrium flows past a simplified Space-Shuttle configuration. AIAA Paper 97-0275 (1997)

    Google Scholar 

  2. M.G. Dunn, S.W. Kang: Theoretical and experimental studies of reentry plasmas. NASA CR-2232 (1973)

    Google Scholar 

  3. R.N. Gupta, J.M. Yoss, R.A. Thompson, K.P. Lee: A review of reaction rates and thermodynamic transport properties for an 11-species air model for chemical and thermal nonequilibrium calculations to 30 000K. NASA-RP-1232 (1990)

    Google Scholar 

  4. K. Hannemann, J. Martinez-Schramm, S. Karl, W. Beck: Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG. AIAA Paper 2002–2913 (2002)

    Google Scholar 

  5. M.K. McIntosh: Computer Program for the Numerical Calculation of Frozen and Equilibrium Conditions in Shock Tunnels. (Australian National University, Canberra A.C.T. 1968)

    Google Scholar 

  6. R.C. Millikan, D.R. White: Systematics of Vibrational Relaxation. Journal of Chem. Physics 39(12), (1963)

    Google Scholar 

  7. C. Park: On convergence of computation of chemically reacting flows. AIAA Paper 85-0247 (1985)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Karl, S., Martinez Schramm, J., Hannemann, K. (2005). Experimental and numerical investigation of high enthalpy flow past a cylinder in HEG. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_24

Download citation

  • DOI: https://doi.org/10.1007/978-3-540-27009-6_24

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-22497-6

  • Online ISBN: 978-3-540-27009-6

  • eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)

Publish with us

Policies and ethics