Acoustic Similarity Laws for Fans

[+] Author and Article Information
W. Neise, B. Barsikow

Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e. V., Institut für Experimentelle Strömungsmechanik, Abteilung Turbulenzforschung, 1000 Berlin 12, West Germany

J. Eng. Ind 104(2), 162-168 (May 01, 1982) (7 pages) doi:10.1115/1.3185811 History: Received July 29, 1981; Online July 30, 2009


In order to verify experimentally acoustic similarity laws for fans, experiments were made with three, dimensionally similar centrifugal fans of 140, 280, and 560 mm impeller diameter. The fans were connected to anechoically terminated discharge ducts. It is shown that the influence of the Reynolds number on the radiated sound pressure is negligible within 1.4•105 ≦ Re ≦ 2.2•106 , which is the range covered by the measurements. This is in agreement with earlier studies in which the Reynolds number was varied from 1.4•104 to 4.5•105 . From the experimental results it is concluded that fan noise data that are taken on model fans can be extrapolated to other dimensionally similar fans of different size for arbitrary fan speeds and working fluids, provided that the operating condition and the measurement position are the same.

Copyright © 1982 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In