4— = a D Figure 3.- Partially open jet. Figure 7.- Static tube with side i orifices. 8 18 16 20 *" um/sek Figure 5.- Velocity distribu- tion at right angles to main flow plane for partial- ly open Jet. Figure 8.- Static pressure tube Figure 6.- Device for rotating the with inside holes. pressure…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.