Numerical investigation of boundary layer separation control on the low-pressure turbine blade by oscillatory blowing-Reference-Cited by-同舟云学术

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Numerical investigation of boundary layer separation control on the low-pressure turbine blade by oscillatory blowing

Published:2024-03 Issue: Volume:146 Page:108961
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Yang PengCheng,Chen ShaoWen^ORCID,Chen ShuaiTong,Liu GuanYu^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference30 articles.

1. Separated flow measurements on a highly loaded low-pressure turbine airfoil;Volino;Volino, R. J.,2008

2. Aerodynamic performance of a very high lift low pressure turbine blade with emphasis on separation prediction;Houtermans;J. Turbomach.,2004

3. Toward the expansion of low-pressure-turbine airfoil design space;Praisner;J. Turbomach.,2008

4. An investigation of reynolds lapse rate for highly loaded low pressure turbine airfoils with forward and Aft loading;Lyall;J. Turbomach.,2012

5. Active flow control for low-pressure turbines;Bons;AIAA Journal,2018

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