Skip to main content

Boundary Layers

  • Chapter
  • First Online:
Blast Waves

Part of the book series: Shock Wave and High Pressure Phenomena ((SHOCKWAVE))

  • 1985 Accesses

Abstract

A boundary layer forms when a fluid flows over a solid surface. The fluid velocity goes to zero at the surface because of the roughness of a real surface. A general definition for a boundary layer is “a region in which the velocity gradient and related shear stresses become large enough that they cannot be neglected.” (Prandtl and Tietjens 1934). Thus the consideration of the effects of a boundary layer is left to the user. Even very highly polished surfaces are rough on the scale of gas molecule separation distances. From Sect. 2.2 on the discussion of sound propagation we showed that the intermolecular distance was approximately 2.e-7 cm for sea level air. The surface would need to be smooth to a few times this distance for the surface to not form a boundary layer.

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 EPUB and 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

References

  • Launder, B.E., Spalding, D.B.: The numerical computation of turbulent flows. Comput. Methods Appl. Mech. Eng. 3, 269 (1974)

    Article  MATH  Google Scholar 

  • Mirels, H.: The wall boundary layer behind a moving shock wave, Grenzschichforschung Symposium, pp. 283–292. Springer, Freiburg (1958)

    MATH  Google Scholar 

  • Mirels, H.: Boundary layer growth behind Mach reflections, 10th Mach Reflection symposium, Abstract Book, Denver, 20–23 July 1992

    Google Scholar 

  • Mixed Company/Middle Gust Results Meeting 13-15 March 1973, Volume 1, Sessions 1, 2A, and 3A, Published by, General Electric Company-Tempo, 1 May 1973

    Google Scholar 

  • Prandtl, Tietjens: Applied Hydro and Aeromechanics, p. 59. Dover, New York (1934)

    MATH  Google Scholar 

  • Sakurai, H., Adachi, T., Kobayashi, S.: Effect of boundary layer on Mach reflection over a wedge, Proceedings of the 22nd international symposium on shock waves. pp. 1249–1252 (2000)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

Copyright information

© 2018 Springer International Publishing AG

About this chapter

Cite this chapter

Needham, C.E. (2018). Boundary Layers. In: Blast Waves. Shock Wave and High Pressure Phenomena. Springer, Cham. https://doi.org/10.1007/978-3-319-65382-2_8

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-65382-2_8

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-65381-5

  • Online ISBN: 978-3-319-65382-2

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics