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Numerical analysis of aerodynamic compensation pitot-static tube

  • Žunić T
  • Dovatov B
  • Nenadić I
Scientific Technical Review (2023) 73(2) 3-6
DOI: 10.5937/str23020032z
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Abstract

Numerical analysis of a flow filed around the aerodynamic compensation pitot-static tube that is used on a domestic ORAO J22 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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APA

Žunić, T., Dovatov, B., & Nenadić, I. (2023). Numerical analysis of aerodynamic compensation pitot-static tube. Scientific Technical Review, 73(2), 3–6. https://doi.org/10.5937/str23020032z

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