Optimization of film hole row locations of a nozzle guide vane using network approach-Reference-Cited by-同舟云学术

Optimization of film hole row locations of a nozzle guide vane using network approach

Published:2020-06-03 Issue:5 Volume:145 Page:2661-2674
ISSN:1388-6150
Container-title:Journal of Thermal Analysis and Calorimetry
language:en
Short-container-title:J Therm Anal Calorim

Author:

Kukutla Pol Reddy,Prasad B. V. S. S. S.,Tarigonda Hariprasad,Reddy D. Raghurami

Publisher

Springer Science and Business Media LLC

Link

https://link.springer.com/content/pdf/10.1007/s10973-020-09841-2.pdf

Reference37 articles.

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2. Francesco B, Mantero M, Gasnier T, Ronconi E. Analysis of heavy duty gas turbine stator-rotor cavity through 3D CFD-1D fluid network field measurements combined approach. In: Proceedings of ASME Turbo Expo, GT2016- 57629, 13–17 June 2016, Seoul, South Korea. https://doi.org/10.1115/gt2016-57629.

3. Gladden, HJ, Livingood JNB. Procedure for scaling of experimental turbine vane airfoil temperatures from low to high gas temperatures. NASA TN D-6510, 1971.

4. Sciubba E. Air-cooled gas turbine cycles part 1: an analytical method for the preliminary assessment of blade cooling flow rates. Energy. 2015;83:104–14.

5. Chandran D, Prasad BVSSS. Conjugate heat transfer study of combined impingement and showerhead film cooling near NGV leading edge. Int J Rotat Mach. 2015;2015:315036.

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