Figure 5 - uploaded by Piyush Pandita
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2D airfoil section of gas turbine last stage blade.
Source publication
Engineering problems that are modeled using sophisticated mathematical methods or are characterized by expensive-to-conduct tests or experiments, are encumbered with limited budget or finite computational resources. Moreover, practical scenarios in the industry, impose restrictions, based on logistics and preference, on the manner in which the expe...
Contexts in source publication
Context 1
... baseline design and operating conditions are derived from an industrial gas turbine last stage blade. Figure 5 shows the 2D section used to design the airfoil. The same has been extracted along a 3D streamline. ...
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