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Tag Archives: nozzle

Design of a Truncated Ideal Nozzle for a Re-usable First Stage Launcher

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusMay 8, 2024

Sebastian KARL, Tamas BYKERK, Mariasole LAURETI

DOI Number: 10.60853/10nj-6656

Conference Number: HiSST-2024-0034

Numerical and experimental investigation of air flow and heat transfer in a complete circuit of a hypersonic wind tunnel

HiSST 2018, Hypersonic Aerodynamics, Testing and Evaluation, Thermal and Energy Management SystemsBy tverminOctober 6, 2023

Drozdov S.M., Davletkildeev R.A., Rtischeva A.S.

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_640800

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