Developed measurement device flow velocity in the test section of the wind tunnel low subsonic speeds, has the advantage over liquid manometers: less inertia, ease of application, clarity of output data, to measure the flow rate fluctuations. The developed device has the potential to become a duplicate anaerobic membrane device existing instruments measuring speed of the aircraft or the main system for small pilotless aircraft.
wind tunnel, experimental studies, flow rate, anemometer, turbulence, dial coordinates, tubeof Pito, sensor of pressure
"Tsyfrovyi prystrii vymiru shvydkosti potoku v robochii chastyni aerodynamichnoi truby malykh dozvukovykh shvydkostei" [Digital device measuring flow rate in the working of small wind tunnel subsonic speeds],
Scientific Works of Kharkiv National Air Force University,