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Volume 12 Issue 07
July 2026
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Author(s)
SS Prithvi Lohith R Lohith DM Karthik BM, Dr.P B shetty
Abstract
In The Present Work The First Stage Rotor Blade Of A Two-stage Gas Turbine Has Been Analyzed For Structural, Thermal Using Commercial Software Which Is Finite Element Software. In The Process Of Getting The Thermal Stresses, The Temperature Distribution I
Keywords
Rotor Blade; Turbine; Failure; Analysis; Aircraft Engine.
Paper ID
IJSARTV4I422614
Publication Date
April 12, 2018
Research Area
Mechanical Engineering