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Part of a CF6-80C2 turbofan engine, owned by Garuda Indonesia, which frequently gets damaged and causes an unscheduled engine removal is turbine blade stage I. Based on failure analysis from the metallurgical viewpoint on the turbine which ruptured, it was reported that the failure happens due to cr...

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Bibliographic Details
Main Author: SASAKAWA ISKANDAR (NIM: 13607048); Pembimbing: Dr. Hendri Syamsudin; Dr. Eng. Arif Sugiant, SILUR
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/17231
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Institution: Institut Teknologi Bandung
Language: Indonesia

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