Hostname: page-component-586b7cd67f-t7fkt Total loading time: 0 Render date: 2024-11-28T17:14:07.462Z Has data issue: false hasContentIssue false
  • English
  • Français

Design and performance of thin, circular arc, wind-tunnel turning vanes

Published online by Cambridge University Press:  03 February 2016

G. Johl ,
M. Passmore  and
P. Render
G. Johl
Affiliation:
Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough, UK
M. Passmore
Affiliation:
Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough, UK
P. Render
Affiliation:
Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough, UK
Get access Rights & Permissions [Opens in a new window]

Extract

Although test rig data exists for ¼ circle turning vanes, the actual performance of these vanes once installed in a wind tunnel, and the extent to which test rig results are replicated, is rarely known. This paper compares pressure loss coefficient and velocity profile data from a vane test module with measurements taken in the low speed wind tunnel described in Ref. 1.

Type
Research Article
Information
The Aeronautical Journal , Volume 111 , Issue 1116 , February 2007 , pp. 115 - 118
Copyright
Copyright © Royal Aeronautical Society 2007 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Johl, G.S., Passmore, M.A. and Render, P.M., Design methodology and performance of an indraft wind tunnel, Aeronaut J, September 2004, 108,(1087), pp 465–473.Google Scholar
2. Klein, G.J., Tupper, K.F. and Green, J.J., The design of corners In fluid channels, Canadian J Research, 3, pp 272–285 (1930).Google Scholar
3. Collar, A.R; Some experiments with cascades of aerofoils, Aeronautical Research Committee Technical Report 1768 (1936).Google Scholar
4. Salter, C., Experiments on thin turning vanes; reports and memoranda No 2469 (Aerodynamics Division NPL); 25 October 1946.Google Scholar
5. Winter, K.G., Comparative tests of thick and thin turning vanes in the Royal Aircraft Establishment 4 x 3ft wind tunnel; Reports and Memoranda No 2589; August 1947.Google Scholar
6. Idelchik, I.E. and Fried, E., Flow Resistance, Hemisphere Publishing Corporation, 1989.Google Scholar