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Tag Archives: Supersonic Split Line Nozzle

Influence of the Swing Angle on the Performance of Planar SSSL Nozzle

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusJune 6, 2024

Rui LI, Jinglei XU, Haiyin LV

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-285

Conference number: HiSST-2024-285

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