Home – Home – Jornals – Thermophysics and Aeromechanics 2017 number 2

The recovery ratio of a wedge-shaped hot-film probe was determined in an experi-mental as well as numerical study, since this information is still unpublished and es-sential for using the probe in hot-film anemometry. The experiments were conducted at the Khristianovich Institute of Theoretical and Applied Mechanics (ITAM) in Novosibirsk, Russia, and the simulations were performed with StarCCM+, a com-mercial 2nd order finite volume code. In the analysis, the Mach number was varied be-tween M = 2 and M = 4, and the unit Reynolds number ranged from Re₁ = 3.8x10⁶ to Re₁ = 26.1x10⁶ m^–1, depending on the Mach number. During the experiment, the stag-nation temperature was kept constant for each Mach number at a separate value in the range of T₀ = 289 x 7 K. Three different stagnation temperatures were used in the simulations: T₀ = 259 K, T₀ = 289 K, and T₀  = 319 K. The difference between the ex-perimental and the numerical results is ≤ 0.5 %, and, therefore, both are in very good accordance. The influence of the Mach number, of the unit Reynolds number, and of the stagnation temperature was analysed, and three different fitting functions for the recovery ratio were established. In general, the recovery ratio shows small varia-tions with all three tested parameters. These dependencies are of the same order of magnitude.