Accuracy of RANS CFD Methods for Design Optimization of Turbine Blade Tip Geometries-Reference-Cited by-同舟云学术

Accuracy of RANS CFD Methods for Design Optimization of Turbine Blade Tip Geometries

Published:2018-07-08 Issue: Volume: Page:
ISSN:
Container-title:2018 Joint Propulsion Conference
language:
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Author:

Paty Marek¹,Lavagnoli Sergio¹

Affiliation:

1. von Kármán Institute for Fluid Dynamics

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4435

Reference23 articles.

1. Comparison of Steady and Unsteady RANS Heat Transfer Simulations of Hub and Endwall of a Turbine Blade Passage

2. P. Vass, “Numerical investigation of the tip leakage flow in different high pressure turbine blade configurations,” Ph.D. thesis,Université Catholique de Louvain, 2012.

3. Investigation of Leakage Flow and Heat Transfer in a Gas Turbine Blade Tip With Emphasis on the Effect of Rotation

4. Winglets for Improved Aerothermal Performance of High Pressure Turbines

5. Heterogeneous Optimization Strategies for Carved and Squealer-Like Turbine Blade Tips

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