Foreign Research Progress

Abstract

In this article, the author gives a detailed description of the Laboratory which possesses a wind‐tunnel for normal aerodynamic research and another for particularly high speeds—the supersonic wind‐tunnel. 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.

Citation

(1944), "Foreign Research Progress", Aircraft Engineering and Aerospace Technology, Vol. 16 No. 11, pp. 327-328. https://doi.org/10.1108/eb031192