NASA NTRS · 19730001745
Development of a three axis fluidic airspeed sensor
Abstract
A three axis fluidic airspeed sensor system has been fabricated and wind tunnel tested. The complete system consists of the fluidic sensor, air power supply and instrumentation and readout. The system is adapted to aircraft and requires only the standard aircraft 28V dc supply to function.
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Neradka, V. F.. 1972-08-01. Development of a three axis fluidic airspeed sensor. https://ntrs.nasa.gov/citations/19730001745
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