Skip to main content

DNS of Boundary-Layer Receptivity to Freestream Sound for Hypersonic Flows Over Blunt Elliptical Cones

  • Conference paper
Recent Advances in DNS and LES

Part of the book series: Fluid Mechanics and its Applications ((FMIA,volume 54))

Abstract

This paper is concerned with the problem of leading-edge receptivity of 3-D hypersonic boundary layers over a blunt elliptical cone. The receptivity of boundary layers to disturbances is the process of converting environmental disturbances into instability waves in the boundary layers. It provides important initial conditions in terms of amplitude, frequency, and phase for the study of development of instability waves in the boundary layers (Goldstein, 1989; Saric, 1994). Most theoretical results on boundary-layer receptivity have been obtained from the asymptotic analysis of incompressible flows. The asymptotic analysis explains how the long wavelength freestream acoustic disturbances enter a boundary layer and generate short-wavelength Tollmien-Schlichting (T-S) waves downstream of the leading edge. Recently, direct numerical simulation (DNS) of the Navier-Stokes equations has been used as a research tool in the studies of stability and transition. Examples of the DNS studies on the receptivity of boundary layers can be found in (Murdock, 1981; Lin, 1992; Buter, 1994: Casalis, 1994; Corke, 1996). Most of these studies have been for incompressible or low-speed compressible boundary layers.

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

  • Buter, T. A. and Reed, H. L., Boundary Layer Receptivity to Free-Stream Vorticity, Physics of Fluids, Vol. 6, No. 10, 1994, pp. 3368–3379.

    Article  ADS  MATH  Google Scholar 

  • Casalis, G. and Cantaloube, B., Receptivity by Direct Numerical Simulation, Direct and Large-Eddy Simulation I, Vol. P. R. Voke et al., editors, pp. 237–248, Kluwer Academic Publishers, 1994.

    Google Scholar 

  • Corke, T. C. and Haddad, O., Receptivity to sound on a parabolic leading edge, In Transitional Boundary Layers in Aeronautics, Vol. Edited by R.A.W.M. Henkes and J. L. van Ingen, pp. 403–412, North-Holland, Amsterdam, 1996.

    Google Scholar 

  • Fay, J. A. and Riddell, F. R., Theory of Stagnation Point Heat Transfer in Dissociated Air, Journal of the Aeronautical Sciences, Vol. 25, 1958, pp. 73–85.

    MathSciNet  Google Scholar 

  • Goldstein, M. E. and Hultgren, L. S., Boundary-Layer Receptivity to Long-Wave Free-Stream Disturbances, Annual Review of Fluid Mechanics, Vol. 21, pp. 137–166 1989.

    Article  MathSciNet  ADS  Google Scholar 

  • Hayes, W. D., The vorticity jump across a gasdynamic discontinuity, Journal of Fluid Mechanics, Vol. 26, 1957, pp. 433–436.

    Google Scholar 

  • Lees, L. and Lin, C. C., Investigation of the Stability of the Laminar Boundary Layer in Compressible Fluid, NACA TN No. 1115, 1946.

    Google Scholar 

  • Lin, N., Reed, H. L., and Saric, W. S., Effect of Leading-Edge Geometry on Boundary-Layer Receptivity to Freestream Sound, Instability, Transition, and Turbulence, Vol. M. Y. Hussaini et al., editors, pp. 421–440, Springer-Verlag, 1992.

    Google Scholar 

  • Murdock, J. W., Tollmien-Schlichting Waves Generated by Unsteady Flow over Parabolic Cylinders, AIAA paper 81-0199, 1981.

    Google Scholar 

  • Saric, W. S., Reed, H. L., and Kerschen, E. J., Leading Edge Receptivity to Sound: Experiments, DNS, and Theory, AIAA Paper 94-2222, 1994.

    Google Scholar 

  • Zhong, X., Direct Numerical Simulation of Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part I: New Numerical Methods and Validation (Invited), AIAA paper 97-0755, 1997.

    Google Scholar 

  • Zhong, X., Direct Numerical Simulation of Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part II: Receptivity to Sound (Invited), AIAA paper 97-0756, January 1997.

    Google Scholar 

  • Zhong, X., High-Order Finite-Difference Schemes for Numerical Simulation of Hypersonic Boundary-Layer Transition, Journal of Computational Physics, Vol. 144, August 1998, pp. 662–709.

    Google Scholar 

  • Zhong, X. and Dong, H., Hypersonic Boundary-Layer Receptivity to Freestream Disturbances Over an Elliptic Cross-Section Cone, AIAA paper 99-0409, 1999.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 1999 Springer Science+Business Media Dordrecht

About this paper

Cite this paper

Zhong, X. (1999). DNS of Boundary-Layer Receptivity to Freestream Sound for Hypersonic Flows Over Blunt Elliptical Cones. In: Knight, D., Sakell, L. (eds) Recent Advances in DNS and LES. Fluid Mechanics and its Applications, vol 54. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-4513-8_43

Download citation

  • DOI: https://doi.org/10.1007/978-94-011-4513-8_43

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-5924-4

  • Online ISBN: 978-94-011-4513-8

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics