Hostname: page-component-686fd747b7-w8rsl Total loading time: 0 Render date: 2025-02-13T13:05:37.005Z Has data issue: false hasContentIssue false
  • English
  • Français

Note on the Temperature Transients in a Supersonic “Blow-Down” Wind Tunnel

Published online by Cambridge University Press:  04 July 2016

L. E. Leavy
L. E. Leavy*
Affiliation:
Wind Tunnels, Aircraft Research Division, A. V. Roe and Co. Ltd.
Get access Rights & Permissions [Opens in a new window]

Extract

In recent years, due to the high cost of continuous supersonic wind tunnels, much attention has been focused on the simpler intermittent “blow-down” tunnel.

Considerable data has been published on most aspects of the design of this type of equipment and quite a number of large installations have recently been brought into operation in the United States, with even larger numbers currently building both in this country and in the United States.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 62 , Issue 572 , August 1958 , pp. 598 - 599
Copyright
Copyright © Royal Aeronautical Society 1958

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.Pillow, A. F. (1952). The Theory of Heat Regenerators in the Unsteady State. Comm. of Australia, Aeronautical Research Lab. Report A78, 1952.Google Scholar
2.Lukasiewicz, J. (1954). Development of Intermittent Wind Tunnel Technique. N.A.E. Ottawa. Paper Presented at A.G.A.R.D. Wind Tunnel and Model Testing Panel, May 1954.Google Scholar
3.Tucker, N. B. (1956). Data on Temperature Stabilisation and Diffuser Performance of the 5 ft. x 5 ft. Pilot Blowdown Wind Tunnel. (N.A.E. Ottawa.) Paper Presented at A.G.A.R.D. Wind Tunnel and Model Testing Panel, August 1956.Google Scholar