Abstract
A convective-film system of high pressure-differential turbine blade cooling is presented. The results of calculating the thermal-hydraulic blade state using the KW3D software are given.
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Original Russian Text © Guanghua Zheng, 2010, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2010, No. 4, pp. 70–72.
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Zheng, G. Development of a high pressure-differential turbine blade cooling system. Russ. Aeronaut. 53, 475–478 (2010). https://doi.org/10.3103/S1068799810040161
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DOI: https://doi.org/10.3103/S1068799810040161