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Tag Archives: Fu–Wang transition model

Effects of Boundary Layer Transition on Dynamic Stability for Hypersonic Blunt-Cone Vehicles

1.Events, 1.HiSST 2025, High-Speed Aerodynamics and Aerothermodynamics with application to hypersonic regimesBy Beata Wierzbińska-PrusOctober 22, 2025Leave a comment

Li Jiahao, Wang Liang, Zhao Rui, Sha Xinguo, Wang Yutang

DOI Number: N/A

Conference number: HiSST-2025-271

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