Full-coverage film cooling: Film effectiveness and heat transfer coefficients for dense hole arrays at different hole angles, contraction ratios, and blowing ratios

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Department of Engineering Science, University of Oxford, Oxford, United Kingdom [1 ]
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Proc. ASME Turbo Expo | / PARTS A AND B卷 / 1707-1723期
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Compilation and indexing terms; Copyright 2025 Elsevier Inc;
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Gas turbines - Heat transfer coefficients - Location - Reynolds number
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