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ISSN: 1820-0206 First published in 1950
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doi:10.5937/str23020032
Vol. 73, No. 2 (2023), Pages: 3-6
Numerical Analysis
of Aerodynamic Compensation Pitot-Static Tube
Tanja Žunić
Numerical analysis of
a flow filed around the aerodynamic compensation pitot-static tube
that is used on a domestic ORAO J-22 aircraft is presented in this
paper. The analysis was performed for three different Mach numbers
of the free stream velocity for two configurations of the
pitot-static tube. The comparison of the pressure coefficient (Cp)
distribution for both of the configurations is given.
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