Effect of Nozzle Pressure and Shape Ratios on Gas Flow of a 122 mm Supersonic Rocket Nozzle investigated by CFD

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dc.contributor.authorChatchapat Chaiaiad
dc.contributor.authorJatuporn Thongsri
dc.date.accessioned2025-07-21T06:09:27Z
dc.date.issued2023-06-25
dc.identifier.doi10.1109/itc-cscc58803.2023.10212737
dc.identifier.urihttps://dspace.kmitl.ac.th/handle/123456789/12599
dc.subjectOverall pressure ratio
dc.subjectRocket (weapon)
dc.subjectRocket engine nozzle
dc.subjectRocket engine
dc.subject.classificationRocket and propulsion systems research
dc.titleEffect of Nozzle Pressure and Shape Ratios on Gas Flow of a 122 mm Supersonic Rocket Nozzle investigated by CFD
dc.typeArticle

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