Optimal Heat Flux Reduction Inside Film Cooled Wall
Author:
Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-80946-1_2
Reference14 articles.
1. Krivonosova V, Lebedev A, Simin N, Zolotogorov M, Kortikov N (2011) Experimental and numerical analysis of high temperature gas turbine nozzle vane and film cooling effectiveness. In: Turbo Expo 2011. GT-45294, Proceedings of ASME. Vancouver, British Columbia, pp 1–9
2. Krivonosova VV, Kortikov NN (2018) Analysis and improvement of the cooling system of a gas turbine nozzle vane. St. Petersburg Polytechnic Univ J Eng Sci Technol 24(03):80–90. https://doi.org/10.18721/JEST.240307
3. Baldauf S, Scheurlen M, Schulz A, Wirtig S (2002) Correlation of film cooling effectiveness from thermographic measurements at engine like conditions. In: Proceeding of ASME. Turbo Expo 2002, Amsterdam, The Netherlands, GT-2002-30180, pp 1–14
4. Baldauf S, Scheurlen M, Schulz A, Wirtig S (2020) Heat flux reduction from film cooling and correlation of heat transfer coefficients from thermographic measurement at engine like conditions. In: Proceedings of ASME. Turbo Expo 2002, Amsterdam, The Netherlands, GT-2002-30181, pp 1–12
5. IOSO NS GT vers. 2.0. IOSO Technology Center. 2001–2003, Moscow. http://www.iosotech.com. Last accessed 21 Nov 2016
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