The Proceedings of Conference of Kansai Branch
Online ISSN : 2424-2756
Session ID : 20412
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Consideration of Cooling Hole Configuration Taking into Account Aerodynamic Losses due to Film Cooling on the Endwall of Gas Turbine Blades
*Itsuki MASUDAMasahiro MIYABE
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[in Japanese]
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© 2024 The Japan Society of Mechanical Engineers
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