Thermostructural Numerical Analysis of the Thrust Chamber of a Liquid Propellant Rocket Engine

The numerical simulation of rocket engine thrust chambers is very challenging as several damaging phenomena, such as plasticity, low-cycle-fatigue (LCF) and creep occur during its service life. The possibility of simulating the thermostructural behavior of the engine, by means of non-linear finite e...

Descripción completa

Detalles Bibliográficos
Autores principales: Citarella, Roberto, Ferraiuolo, Michele, Perrella, Michele, Giannella, Venanzio
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9370048/
https://www.ncbi.nlm.nih.gov/pubmed/35955363
http://dx.doi.org/10.3390/ma15155427

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9370048/
https://www.ncbi.nlm.nih.gov/pubmed/35955363
http://dx.doi.org/10.3390/ma15155427

Ejemplares similares