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Optimization of a fan-shaped hole to improve film cooling performance by RBF neural network and genetic algorithm

  • Published:2016-11 Issue: Volume:58 Page:18-25
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Wang Chunhua,Zhang Jingzhou,Zhou Junhui

Funder

Natural Science Fund Program of China

Fundamental Research Funds for the Central Universities

Postdoctoral Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. A review of shaped hole turbine film-cooling technology;Bunker;J. Heat Transfer,2005

2. Investigation on film cooling characteristics from a row of converging slot-holes on flat plate;Yao;Sci. China, Technol. Sci.,2011

3. Effect of upstream step on flat plate film-cooling effectiveness using PSP;Rallabandi;J. Turbomach.,2011

4. Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits;Gritsch;J. Turbomach.,1998

5. Effects of hole shape on film cooling with large angle injection;Kohli,1999

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