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.
Foreign Research Progress
Aircraft Engineering and Aerospace Technology ; 16 , 11 ; 327-328
1944-11-01
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1943
Emerald Group Publishing | 1944
Emerald Group Publishing | 1943
Emerald Group Publishing | 1945
Emerald Group Publishing | 1944