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Foreign Research Progress

Foreign Research Progress In this article, the author gives a detailed description of the Laboratory which possesses a windtunnel for normal aerodynamic research and another for particularly high speedsthe supersonic windtunnel. The normal tunnel has several points of interest it can be used cither open or closed and, in the latter case, it is possible to achieve a particularly good pressure distribution. The controls and measuring devices are described. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Foreign Research Progress

Aircraft Engineering and Aerospace Technology , Volume 16 (11): 2 – Nov 1, 1944
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031192
Publisher site
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Abstract

In this article, the author gives a detailed description of the Laboratory which possesses a windtunnel for normal aerodynamic research and another for particularly high speedsthe supersonic windtunnel. The normal tunnel has several points of interest it can be used cither open or closed and, in the latter case, it is possible to achieve a particularly good pressure distribution. The controls and measuring devices are described.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Nov 1, 1944

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