Measurements with Honeycombs in the Full-Scale and in the Model Vertical Wind Tunnel
Report Number: WADC TR 52-207 Author: Knackstedt, Wilhelm F. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1952-08 Pages: 23 AD Number: AD0008717 Original AD Number: 8717Contrails does not possess a copy of this report. Click here to offer Contrails a donation of this report
Abstract: Measurements in the full-scale Vertical Wind Tunnel and in a 1:12 scale model of this tunnel were made to determine if a dynamic pressure distribution required for the spinning of airplane models could be achieved by a honeycomb of cozrventional type. Test results indicate that a minor change of the nozzle contour at the place where the honeycomb is installed is a possible means to obtain the required dynamic pressure distribution.