Abstract
A nontraditional method is proposed for measuring the total pressure behind the compressor rotor in relative motion of the gas flux. The operation of a rotary probe is considered. The flow pattern at the exit from the rotor’s blade channel is determined.
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Original Russian Text © V.Yu. Aleksandrov, K.K. Klimovskii, 2013, published in Vestnik Mashinostroeniya, 2013, No. 12, pp. 13–17.
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Aleksandrov, V.Y., Klimovskii, K.K. Measuring the total pressure in the relative motion of the flux behind a compressor rotor. Russ. Engin. Res. 34, 127–130 (2014). https://doi.org/10.3103/S1068798X14030046
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DOI: https://doi.org/10.3103/S1068798X14030046