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The European transonic wind-tunnel ETW: A cryogenic solution

Published online by Cambridge University Press:  04 July 2016

J. P. Hartzuiker
J. P. Hartzuiker*
Affiliation:
Technical Group, European Transonic Wind-tunnel
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Extract

The history of the European Transonic Wind-tunnel is briefly described.

After a discussion of the tunnel specifications and performance, a general description of the facility is provided.

The results of an investigation into the expected future use of the tunnel are summarised.

Information on the pilot tunnel PETW is presented, as well as some results on flow quality obtained in an aerodynamic test rig.

Finally, some reference is made to a supporting programme on cryogenic technology.

Type
Research Article
Information
The Aeronautical Journal , Volume 88 , Issue 879 , November 1984 , pp. 379 - 394
Copyright
Copyright © Royal Aeronautical Society 1984 

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References

1. Hartzuiker, J. P. Küchemann’s role in the promotion of new windtunnels — in ‘Towards new transonic Windtunnels’, AGARD-AG-240,1979.Google Scholar
2. Hartzuiker, J. P. The need for large windtunnels in Europe. Report of the Large Windtunnels Working Group, AGARD-AR- 60, 1972.Google Scholar
3. Hartzuiker, J. P. The need for large transonic windtunnels in Europe. Second report of the Large Windtunnels Working Group, AGARD-AR-70,1974.Google Scholar
4. Hartzuiker, J. P., Christophe, J., Lorenz-Meyer, W. and Pugh, P. G. The cryogenic Windtunnel; another Option for the European transonic Facility — in Towards new transonic Windtunnels’, AGARD-AG-240,1979.Google Scholar
5. Kilgore, R. A., Goodyer, M. J., Adcock, J. B. and Davenport, E. E. The cryogenic Windtunnel Concept for high Reynolds Number Testing. NASA TN-D 7762,1974.Google Scholar
6. Hartzuiker, J. P., Christophe, J., Lorenz-Meyer, W. and Pugh, P. G. Recommendation on the Drive System for the European high-Reynolds-Number transonic Windtunnel. Defence Research Group AC/243(PG. 7/WG.l) D/10,1976.Google Scholar
7. Hartzuiker, J. P., Pugh, P. G., Lorenz-Meyer, W. and Fasso, G. E. On the Flow Quality necessary to the large European high-Reynolds-Number transonic Windtunnel LEHRT. AGARD-R-644.1976.Google Scholar
8. North, R. J. The cryogenic Technology Programme of the European transonic Windtunnel Project. First International Symposium on Cryogenic Wind Tunnels, 1979.Google Scholar
9. McKinney, L. W. and North, R. J. Report of the Conveners Group on cryogenic Test Technology, AGARD-AR-174,1982.Google Scholar