HEAT TRANSFER ANALYSIS OF GAS TURBINE BLADES

• Author(s):

  Madhusudhan N | Nithin A | Prajwal J N | Sadat Khan

• Keywords:

  Cooling, Circular Holes, Hexagonal Holes, Turbine Blades

• Abstract:

  Cooling Of Gas Turbine Blades Is A Major Consideration In The Design Of Gas Turbine Blades Due To High Operating Temperature Working Conditions For Greater Thermal Efficiency For The Stage. Several Methods Of Cooling Of Gas Turbine Blades Coupled With Inn

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Other Details

• Paper id:

  IJSARTV4I422739

• Published in:

  Volume: 4 Issue: 4 April 2018

• Publication Date:

  2018-04-16

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