Skip to main content

Low-Speed Aerodynamics

  • Chapter
Flight Physics

In the history of aviation, flight speeds have constantly increased due to the development of more powerful engines and the improvement of aerodynamic properties. Especially, the introduction of jet engines and sweptback wings made it possible to approach and even exceed the speed of sound. This sonic speed, the propagation speed of very small pressure disturbances in the atmosphere, plays an important role in determining which flow phenomena will occur. In the low-speed range, all flow velocities around the aeroplane are significantly smaller than the speed of sound. The pressure disturbances caused by the aircraft can propagate forward – in a way the air is “warned of” the oncoming aircraft – and the air particles recede for the leading edge of a wing or the nose of a body. This is no longer the case when the flight speed exceeds the speed of sound. Then the flow pattern is greatly changed by the occurrence of shock waves, nearly discontinuous pressure changes. These are caused by the compressibility of the atmospheric air, that is, the ability of air to change specific volume and density with increasing pressure.

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 39.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 54.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 79.99
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.

Bibliography

  1. Anderson Jr., J.D., A History of Aerodynamics, Cambridge Aerospace Series 8, Cambridge University Press, Cambridge, UK, 1998.

    MATH  Google Scholar 

  2. Anderson Jr., J.D., Fundamentals of Aerodynamics, Second Edition, McGraw-Hill, Inc., New York, 1991

    Google Scholar 

  3. Clancy, L.J., Aerodynamics, Pitman Aeronautical Engineering Series, Pitman Publishing, London, John Wiley & Sons, New York, 1975.

    Google Scholar 

  4. Dubs, F., Aerodynamik der reinen Unterschallströhmung, Birkhäuser-Verlag, Basel, Boston, Stuttgart, 1979.

    Google Scholar 

  5. Glauert, H., The Elements of Aerofoil and Airscrew Theory, Cambridge University Press, Cambridge, UK, 1983.

    Google Scholar 

  6. Hoerner, S.F., Fluid Dynamic Drag, Published by the Author, LCCCN 64-19666, 1965.

    Google Scholar 

  7. Houghton, E.L. and N.B. Carruthers, Aerodynamics for Engineering Students, Third Edition, Edward Arnold, London, 1988.

    Google Scholar 

  8. Katz, J., and A. Plotkin, Low-Speed Aerodynamics, Second Edition, Cambridge University Press, Cambridge, UK, 2001.

    MATH  Google Scholar 

  9. Schlichting, H., Boundary Layer Theory, Seventh Edition, McGraw-Hill Book Company, New York, 1979.

    MATH  Google Scholar 

  10. Smits, A.J., A Physical Introduction to Fluid Dynamics, John Wiley & Sons, Inc., New York, 2000.

    Google Scholar 

Download references

Rights and permissions

Reprints and permissions

Copyright information

© 2009 Springer Science+Business Media, B.V.

About this chapter

Cite this chapter

(2009). Low-Speed Aerodynamics. In: Flight Physics. Springer, Dordrecht. https://doi.org/10.1007/978-1-4020-8664-9_3

Download citation

  • DOI: https://doi.org/10.1007/978-1-4020-8664-9_3

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-1-4020-8663-2

  • Online ISBN: 978-1-4020-8664-9

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics