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

Thumbnail Image

Date

2023-06-25

Authors

Journal Title

Journal ISSN

Volume Title

Publisher

Abstract

Description

Keywords

Overall pressure ratio, Rocket (weapon), Rocket engine nozzle, Rocket engine

Citation

URI

https://dspace.kmitl.ac.th/handle/123456789/12599

Collections

All

Endorsement

Review

Supplemented By

Referenced By