About this document
Thermal Stress Analysis of Rocket Nozzle by பொன்னியின் செல்வன் is a document available to read on EtoBox.
The document summarizes a study that used finite element analysis to model the thermal stresses in the graphite throat insert of a solid rocket motor nozzle. The analysis solved the transient heat conduction equation using finite elements with temperature-dependent material properties. It calculated temperature distributions over time, then used these results to determine displacements and thermal stresses. The developed computer codes were validated against analytical solutions and ANSYS. The goal was to i
- Author
- பொன்னியின் செல்வன்
- Language
- EN