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Volume 12 Issue 07
July 2026
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Author(s)
Madhusudhan N Nithin A Prajwal J N Sadat Khan
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
Keywords
Cooling
Circular Holes
Hexagonal Holes
Turbine Blades
Paper ID
IJSARTV4I422739
Publication Date
April 16, 2018
Research Area
Mechanical Engineering