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Tag Archives: Turbine based combined cycle engine

Design Study of a 2-dimensional Scramjet Inlet Operating over a Wide Range of Mach Numbers

1.Events, 1.HiSST 2025, Propulsion Systems & ComponentsBy Beata Wierzbińska-PrusOctober 22, 2025Leave a comment

Masahiro TAKAHASHI, Tatsushi ISONO, Koichiro TANI, Sadatake TOMIOKA

DOI Number: N/A

Conference number: HiSST-2025-229

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