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.
A Quasi-Spherical Air Pressure Probe
Russian Aeronautics ; 61 , 2 ; 265-270
2018-04-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch