Optimization Turbine Blade Cooling by Applying Jet Impingement Cooling Channels

1. Ackert, S. (2011) Engine Maintenance Concepts for Financiers Elements of Turbofan Shop Maintenance Costs. 43 pages. PDF available at: http://www.aircraftmonitor.com/uploads/1/5/9/9/15993320/engine_mx_concepts_for_financiers___v2.pdfSearch in Google Scholar

2. Brown, G.O. (2002) The History of the Darcy-Weisbach Equation for Pipe Flow Resistance, in Environmental and Water Resources History. Reston, VA: American Society of Civil Engineers, pp. 34–43. https://doi.org/10.1061/40650(2003)4.Search in Google Scholar

3. Coletti, F., Scialanga, M. and Arts, T. (2012) Experimental Investigation of Conjugate Heat Transfer in a Rib-Roughened Trailing Edge Channel with Crossing Jets, Journal of Turbomachinery, 134(4). https://doi.org/10.1115/1.4003727.Search in Google Scholar

4. Elmenshawy, A.A.A.E. and Alomar, I. (2022) Statistics and Investigation of CF6 Jet Engines Hot Section Failures, pp. 88–98. https://doi.org/10.1007/978-3-030-96196-1_9.Search in Google Scholar

5. Fluent 6.2 Documentation File, ANSYS Manual. (2006).Search in Google Scholar

6. Hylton, L.D. and York, R.E. (1985) Analytical and Experimental Evaluation of the Heat Transfer Distribution Over the Surfaces of Turbine Vanes.Search in Google Scholar

7. Nikora, V. (2006) Hydrodynamics of aquatic ecosystems. Acta Geophysica, 55(1), 3–10. DOI:10.2478/s11600-006-0043-6Open DOISearch in Google Scholar

8. Nirmalan, V. and Hylton, L.D. (1989) An Experimental Study of Turbine Vane Heat Transfer with Leading Edge and Downstream Film Cooling. Heat Transfer; Electric Power; Industrial and Cogeneration. American Society of Mechanical Engineers, 4. https://doi.org/10.1115/89-GT-69.Search in Google Scholar

9. Nozhnitsky, Y.A. (2018) The Problem of Ensuring Reliability of Gas Turbine Engines, IOP Conference Series: Materials Science and Engineering, 302, p. 012082. https://doi.org/10.1088/1757-899X/302/1/012082.Search in Google Scholar

10. Organ, A.J. (2007) Counter-flow spiral heat exchanger – Spirex, The Air Engine. Elsevier, 29–38. https://doi.org/10.1533/9781845693602.1.29.Search in Google Scholar

11. Rossman, C.D. (2016) Analysis of a Coupled Micro- and Triple-Impingement Cooling Analysis of a Coupled Micro- and Triple-Impingement Cooling Configuration in the C3X Vane Configuration in the C3X Vane. Available at: https://commons.erau.edu/edt.Search in Google Scholar

12. Uysal, U. et al. (2006) Heat Transfer on Internal Surfaces of a Duct Subjected to Impingement of a Jet Array with Varying Jet Hole-Size and Spacing, Journal of Turbomachinery, 128(1), 158–165. https://doi.org/10.1115/1.2101859.Search in Google Scholar

13. Wang, J., Sundén, B., Zeng, M., and Wang, Q. (2015) Film cooling effects on the tip flow characteristics of a gas turbine blade, Propulsion and Power Research, 4(1), 9–22, https://doi.org/10.1016/j.jppr.2015.02.003.Search in Google Scholar

14. Wang, K., Li, H. and Zhu, J. (2014) Experimental study of heat transfer characteristic on jet impingement cooling with film extraction flow, Applied Thermal Engineering, 70(1), 620–629. https://doi.org/10.1016/j.applthermaleng.2014.05.077.Search in Google Scholar

15. Yamane, Y. et al. (2012) Effect of Injection Parameters on Jet Array Impingement Heat Transfer, International Journal of Gas Turbine, Propulsion and Power Systems, 4(1), 27–34. https://doi.org/10.38036/jgpp.4.1_27.Search in Google Scholar

16. Zaretsky, E. V., Litt, J. S., Hendricks, R C., Soditus, S M. (2013) Determination of Turbine Blade Life from Engine Field Data. Available at: https://ntrs.nasa.gov/search.jsp?R=20120007098.Search in Google Scholar