EFFECT OF HOLDING TIME AND COOLING RATE ON THE MICROSTRUCTURE OF RENE 142 SUPERALLOY
Nickel-based superalloys are the material used for turbine blades in airplane engines as they are designed to withstand creep. Consequently, gamma prime precipitates within the microstructure of these alloys will change in shape and size that will affect its operational lifetime. Thus, heat treatmen...
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| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/68276 |
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| 機構: | Institut Teknologi Bandung |
| 語言: | Indonesia |