An Artificial Neural Network (Ann) Based Aerothermal Optimization of Film Cooling Hole Locations on the Squealer Tip of an Hp Turbine Blade-Reference-Cited by-同舟云学术

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An Artificial Neural Network (Ann) Based Aerothermal Optimization of Film Cooling Hole Locations on the Squealer Tip of an Hp Turbine Blade

Published:2022 Issue: Volume: Page:
ISSN:1556-5068
Container-title:SSRN Electronic Journal
language:en
Short-container-title:SSRN Journal

Author:

Yıldız Faruk,Alpman Emre,Kavurmacioglu Levent,Camci Cengiz

Publisher

Elsevier BV

Subject

General Earth and Planetary Sciences,General Environmental Science

Reference52 articles.

1. Gas Turbine Heat Transfer and Cooling Technology

2. Blade tip leakage flow and heat transfer with pressure-side winglet;A K Saha;International Journal of Rotating Machinery,2006

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

4. Numerical simulation of film cooling on the tip of a gas turbine blade;S Acharya;Turbo Expo: Power for Land, Sea, and Air,2002

5. Comparison of turbine tip leakage flow for flat tip and squealer tip geometries at high-speed conditions;N L Key;Journal of Turbo-machinery,2006

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