Evaluating the effects of multiple hole profiles on gas turbine blade cooling rate: a computational study
Author:
Publisher
Springer Science and Business Media LLC
Subject
Industrial and Manufacturing Engineering,Modeling and Simulation
Link
https://link.springer.com/content/pdf/10.1007/s12008-023-01418-1.pdf
Reference31 articles.
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2. Kim, K.M., Park, J.S., Lee, D.H., Lee, T.W., Cho, H.H.: Analysis of conjugated heat transfer, stress and failure in a gas turbine blade with circular cooling passages. Eng. Fail. Anal. 18(4), 1212–1222 (2011). https://doi.org/10.1016/j.engfailanal.2011.03.002
3. Yelamasetti, B., Manikyam, S., Kumar, R., Saxena, K.K.: Finite element simulation for predicting temperature and residual stresses distribution developed in dissimilar welds of Monel 400 and AISI 309L. Adv. Mater. Process. Technol. 8(5), 1–11 (2022). https://doi.org/10.1080/2374068X.2021.1948702
4. Bunker, R.S.: A review of shaped hole turbine film-cooling technology. J. Heat Transf. 127(4), 441–453 (2005). https://doi.org/10.1115/1.1860562
5. Bogard, D.G., Thole, K.A.: Gas turbine film cooling. J. Propuls. Power 22(2), 249–270 (2006). https://doi.org/10.2514/1.18034
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