Impact Factor
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Call For Paper
Volume 12 Issue 07
July 2026
Author(s)
Ramanjanayulu.B K A.Swamynath
Abstract
The Innovation Of Cooling Gas Turbine Parts Through Inside Convective Streams Of Single-stage Gasses Has Created Throughout The Years From Basic Smooth Cooling Entries To Exceptionally Complex Geometries Including Many Varying Surfaces. To Accomplish High
Keywords
Heat Transfer Co-efficient
Reynolds Number And Nusselt Number.
Paper ID
IJSARTV3I38422
Publication Date
March 1, 2017
Research Area
Mechanical Engineering