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.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Nov 1, 1944