FAILURE ANALYSIS OF TURBOJET GAS TURBINE BLADES USED IN FIGHTER AIRCRAFT

• Author(s):

  SS Prithvi | Lohith R | Lohith DM | Karthik BM, Dr.P B shetty

• Keywords:

  Rotor Blade; Turbine; Failure; Analysis; Aircraft Engine.

• 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

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Other Details

• Paper id:

  IJSARTV4I422614

• Published in:

  Volume: 4 Issue: 4 April 2018

• Publication Date:

  2018-04-12

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