Boundary Layer Transition Mechanisms in a High-Speed Low-Pressure Turbine Blade

Publication Details

Journal
Open Repository and Bibliography (University of Liège)
Published
2025-09-01
Primary Topic
Turbomachinery Performance and Optimization
Type
article
Field-Weighted Citation Impact
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article

Boundary Layer Transition Mechanisms in a High-Speed Low-Pressure Turbine Blade

Open Repository and Bibliography (University of Liège)
Turbomachinery Performance and Optimization
article

Boundary Layer Transition Mechanisms in a High-Speed Low-Pressure Turbine Blade

article en

Abstract

No abstract available for this paper.
Open Repository and Bibliography (University of Liège)
Affordable and clean energy
Openalex Percentile: Top 27%
Turbomachinery Performance and Optimization
Open Access PDFOpenAlex
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Boundary Layer Transition Mechanisms in a High-Speed Low-Pressure Turbine Blade · Open Repository and Bibliography (University of Liège) (2025) | TGRS Research Map | TGRS