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

• मुख्य लेखकों: Muhammad, M. A. (लेखक), Salleh, Z. (लेखक), Hamid, A. H. A. (लेखक), Sujana, M. J. (लेखक), Kamaludin, K. (लेखक)
• स्वरूप: पुस्तक
• प्रकाशित: Smart Manufacturing Research Institute (SMRI), 2022-09.
• विषय: Article; PeerReviewed
• ऑनलाइन पहुंच: Link Metadata

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...