A genetic algorithm based aerothermal optimization of tip carving for an axial turbine blade-Reference-Cited by-同舟云学术

A genetic algorithm based aerothermal optimization of tip carving for an axial turbine blade

Published:2019-11 Issue: Volume:143 Page:118419
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Maral H.,Alpman E.,Kavurmacıoğlu L.,Camci Cengiz^ORCID

Funder

TAI – Turkish Aerospace Industries Inc.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference34 articles.

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2. Winglets for improved aerothermal performance of high pressure turbines;Coull;J. Turbomach.,2014

3. The effect of blade tip geometry on the tip leakage flow in axial turbine cascades;Heyes;J. Turbomach.,1992

4. Aerothermal investigations of tip leakage flow in axial flow turbines—part I: effect of tip geometry and tip clearance gap;Krishnababu;J. Turbomach.,2008

5. Effect of squealer geometry arrangement on a gas turbine blade tip heat transfer;Azad;J. Heat Transfer,2002

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