Finite element analysis for rocket motor case under internal pressure and thermal loads / M. A. Muhammad ... [et al.]

Rocket motor combustion chamber needs to contain very high pressure and temperature due to burning of rocket fuels. For that reason, the combustion chamber is required to withstand the stresses caused by the static and thermal load generated by the burning of the rocket fuels. History demonstrated t...

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Bibliographic Details
Main Authors: Muhammad, M. A., Salleh, Z., Hamid, A. H. A., Sujana, M. J., Kamaludin, K.
Format: Article
Language:English
Published: Smart Manufacturing Research Institute (SMRI) 2022
Online Access:https://ir.uitm.edu.my/id/eprint/74443/2/74443.pdf
https://ir.uitm.edu.my/id/eprint/74443/
https://jaeds.uitm.edu.my/
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