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...
Saved in:
Main Authors: | Muhammad, M. A. (Author), Salleh, Z. (Author), Hamid, A. H. A. (Author), Sujana, M. J. (Author), Kamaludin, K. (Author) |
---|---|
Format: | Book |
Published: |
Smart Manufacturing Research Institute (SMRI),
2022-09.
|
Subjects: | |
Online Access: | Link Metadata |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Transient thermal analysis of solid propellant rocket motor / Dr. Ts. Ahmad Hussein Abdul Hamid ... [et al.]
by: Abdul Hamid, Ahmad Hussein, et al.
Published: (2022) -
Numerical solution for one dimensional thermal problems using the finite element method / Hisham Md. Basir
by: Md. Basir, Hisham
Published: (2002) -
Finite Element Analysis
Published: (2010) -
Finite Elements and Symmetry
Published: (2020) -
Finite element simulation of polymethyl-acrylamid foam-filled aluminum 2024-t4 tube under dynamic axial loading / Akbar Othman and Mohd Fahrul Hasan
by: Othman, Akbar, et al.
Published: (2012)