Designing a Process for Making Turbine Blades from a Nickel-based Superalloy We are tasked with Jesigning a proxess lior making turbine blades, linon a Nickel-based xuperalloy: The specilic alloy we will be using is a cocumon one in yas turbine engine applicalions knorin as 1N718, which coclains hight levels of nicke], chromium, nnd molybienum. The first step in the design process is to select the approprinte alloy for the application. In this case, we hnve choeen TN718 due to its excellent high-temperzature strength and corrosion resistance. 1. Sesarch thee aspects about this material properties and structure related to the content of our conrse, aud conument 1t. Strain Hardening The next step is to determine the desired level of strain hardening for the blatex. Strain hanjening is a process by which the material is mate stronger by cold woxking, wr deforming the material at low temperatures. The degres af strain hartlening is usually expresset as a gertentage of cold wark. Figure 2, repescuts the cvolution of DN718 rochanical propertics with respece to the gercentage of cold work