The Proceedings of Mechanical Engineering Congress, Japan
Online ISSN : 2424-2667
ISSN-L : 2424-2667
2020
Session ID : J05112
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Application of Compressible Immersed Boundary Method on a Flow of a Fuel-Injector of an Aircraft Engine
*Younghwa CHORahul BALETakeo ODANobuyuki OSHIMA
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© 2020 The Japan Society of Mechanical Engineers
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