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Tag Archives: Turbine Based Combined Cycle

Two-dimensional numerical analysis of the effect of turbo-ramjet nozzle geometry on scramjet thrust performance in a TBCC engine

1.Events, 1.HiSST 2025, Propulsion Systems & ComponentsBy Beata Wierzbińska-PrusOctober 26, 2025Leave a comment

Mika EDAHIRO, Akiko MATSUO, Tatsushi ISONO, Masahiro TAKAHASHI, Sadatake TOMIOKA

DOI Number: N/A

Conference number: HiSST-2025-009

Verification of Variable Inlet Design through Wind Tunnel Test

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusMay 9, 2024

Young Jin KIM, Hyoung Jin LEE

DOI Number: N/A
Conference Number: HiSST-2024-041

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