Study to extend range of calibration Mach numbers and to assess effects of presence of temperature element; error curves for pitot-static pressure measurements and flow direction vane correction curves for range of angles of attack and sideslip are presented.
Wind-tunnel calibrations of combined pitot-static tube, vane-type flow-direction transmitter, and stagnation-temperature element at Mach numbers from 0.60 to 2.87
NASA -- Tech Note
1959
26 pages
Report
Englisch
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