Abstract
This paper considers an air pressure probe, the head part of which is made in the form of a polyhedron inscribed into a sphere. Wind tunnel testing of the probe models is performed, a mathematical model and an algorithm are constructed to calculate all the altitude and airspeed parameters, and an error estimation is given.
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Original Russian Text © M.A. Golovkin, A.A. Efremov, V.V. Sysoev, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 2, pp. 112–116.
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Golovkin, M.A., Efremov, A.A. & Sysoev, V.V. A Quasi-Spherical Air Pressure Probe. Russ. Aeronaut. 61, 265–270 (2018). https://doi.org/10.3103/S1068799818020162
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DOI: https://doi.org/10.3103/S1068799818020162