3D Numerical Simulation to Determine Liner Wall Heat Transfer and Flow through a Radial Swirler of an Annular Turbine Combustor

3D Numerical Simulation to Determine Liner Wall Heat Transfer and Flow through a Radial Swirler of an Annular Turbine Combustor

RANS models in CFD are used to predict the liner wall heat transfer characteristics of a gas turbine annular combustor with radial swirlers, over a Reynolds number range from 50,000 to 840,000. A three dimensional hybrid mesh of around twenty five million cells is created for a periodic section of a...

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Bibliographic Details
Main Author: Kumar, Vivek Mohan
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2015
Subjects:
RANS
K Epsilon
RNG
Swirl
Radial Swirler
Annular Combustor
Nusselt Augmentation
Heat Transfer
Industrial Application
Online Access:http://hdl.handle.net/10919/51949

Internet

http://hdl.handle.net/10919/51949

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