%0 Journal Article
	%A C. Ardil
	%D 2014
	%J International Journal of Aerospace and Mechanical Engineering
	%B World Academy of Science, Engineering and Technology
	%I Open Science Index 96, 2014
	%T Modeling of Temperature Fields of Gas Turbine Blades by Considering Heat Flow and Specified Temperature
	%U https://publications.waset.org/pdf/10008387
	%V 96
	%X A new mathematical model for calculating the temperature field of the profile part of the cooled blades of gas turbines is developed. The theoretical substantiation of the method is based on the application of the method of potential theory (the method of boundary integral equations). The effectiveness of the implementation of the developed mathematical model is confirmed on the basis of a computational experiment.
	%P 2150 - 2155