Digital Particle Image Visualization of the Cooling Film Formation in a Flow Around the Leading Edge of a Vane in a Gas Turbine Engine
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Publisher
Pleiades Publishing Ltd
Link
https://link.springer.com/content/pdf/10.1134/S0040601524700137.pdf
Reference28 articles.
1. R. J. Goldstein, “Film cooling,” Adv. Heat Transfer 7, 321–379 (1971). https://doi.org/10.1016/S0065-2717(08)70020-0
2. S. V. Veretennikov, “Effect of the direction of coolant supply to holes on the vortical structures formed in screen cooling,” Heat Transfer Res. 37, 527–540 (2006). https://doi.org/10.1615/HeatTransRes.v37.i6.50
3. S. I. Sendyurev, A. S. Tikhonov, V. T. Khairulin, and N. Yu. Samokhvalov, “Modern nozzle blade cooling systems for gas turbines under high load,” Vestn. PNIPU, Aerokosm. Tekh., No. 42, 34–46 (2015). https://doi.org/10.15593/2224-9982/2015.42.03
4. S. V. Veretennikov and O. A. Evdokimov, “Visualization and PIV-study of the formation of a cooling film when flowing around the leading edge of the gas turbine nozzle blade,” J. Phys.: Conf. Ser. 1421, 012043 (2019). https://doi.org/10.1088/1742-6596/1421/1/012043
5. J. Westerweel, Digital Particle Image Velocimetry: Theory and Application (Delft Univ. Press, Delft, 1993).
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