Hostname: page-component-78c5997874-xbtfd Total loading time: 0 Render date: 2024-11-09T12:34:51.818Z Has data issue: false hasContentIssue false
  • English
  • Français

An Intermittent High-Reynolds-Number Wind Tunnel

Published online by Cambridge University Press:  07 June 2016

J L Stollery  and
A V Murthy
J L Stollery
Affiliation:
Cranfield Institute of Technology
A V Murthy
Affiliation:
National Aeronautical Laboratory, Bangalore
Get access

Summary

The paper suggests a simple method of generating intermittent reservoir conditions for an intermittent, cryogenic wind tunnel. Approximate performance estimates are given and it is recommended that further studies be made because this type of tunnel could be valuable in increasing the opportunities for research at high Reynolds numbers.

Type
Research Article
Information
Aeronautical Quarterly , Volume 28 , Issue 4 , November 1977 , pp. 259 - 264
Copyright
Copyright © Royal Aeronautical Society. 1977

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 Various authors (see the individual papers) AGARD Fluid Dynamics Panel symposium “Wind-Tunnel Design and Testing Techniques”, London, October 1975.Google Scholar
2 Hartzuiker, J P Christophe, J Lorenz-Meyer, W Pugh, P G Recommendation on the drive system for the European high-Reynolds-number transonic wind tunnel. ARC 37 283, 1976.Google Scholar
3 Oldfield, M L G Jones, T V Schultz, D L A Ludwieg tube with light-piston isentropic compression heating. ARC 34 255, 1973.Google Scholar
4 Jones, T V Schultz, D L Hendley, A D On the flow in an isentropic light-piston tunnel. ARC R & M 3731, 1973.Google Scholar