Optimisation of a turbine inlet guide vane by gradient-based and metamodel-assisted methods-Reference-Cited by-同舟云学术

Optimisation of a turbine inlet guide vane by gradient-based and metamodel-assisted methods

Published:2019-08-09 Issue:6-7 Volume:33 Page:302-316
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Aissa Mohamed Hassanine¹^ORCID,Maffulli Roberto²,Mueller Lasse¹,Verstraete Tom¹

Affiliation:

1. Von Karman Institute for Fluid Dynamics, Sint-Genesius-Rode, Belgium

2. Department of Engineering Science, University of Oxford, Oxford, UK

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/10618562.2019.1683168

Reference48 articles.

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2. A comparative study of kriging variants for the optimization of a turbomachinery system

3. Brooks, C., A. Forrester, A. Keane, and S. Shahpar. 2011. “Multi-Fidelity Design Optimisation of a Transonic Compressor Rotor.” 9th European Turbomachinery Conference, Istanbul, Turkey, March 21–25.

4. Multimodality and Global Optimization in Aerodynamic Design

5. The Trailing Edge Loss of Transonic Turbine Blades

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