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Volume 12 Issue 07
July 2026
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Author(s)
G. Sri latha G.Leela Siva Rama Prasad
Abstract
Cooling Of Gas Turbine Blades Is A Major Consideration Because They Are Subjected To High Temperature Working Conditions. Several Methods Have Been Suggested For The Cooling Of Blades And One Such Technique Is To Have Radial Holes To Pass High Velocity Co
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Paper ID
IJSARTV4I422634
Publication Date
April 13, 2018
Research Area
Mechanical Engineering